Category Praxis Manned Spaceflight Log 1961-2006

STS-109

Int. Designation

2002-010A

Launched

1 March 2002

Launch Site

Pad 39A, Kennedy Space Center, Florida

Landed

12 March 2002

Landing Site

Runway 33, Shuttle Landing Facility, KSC, Florida

Launch Vehicle

OV-102 Columbia/ET-112/SRB BI-111/SSME #1 2056;

#2 2053; #3 2047

Duration

10 days 22 hrs 11 min 9 sec

Call sign

Columbia

Objective

4th Hubble Service Mission (HST SM 3B)

Flight Crew

ALTMAN, Scott Douglas, 42, USN, commander, 3rd mission Previous missions: STS-90 (1998); STS-106 (2000)

CAREY, Duane Gene, 44, USAF, pilot

GRUNSFELD, John Mace, 43, civilian, mission specialist 1, payload commander, 4th mission

Previous missions: STS-67 (1995); STS-81 (1997); STS-103 (1999)

CURRIE, Nancy Jane, 43, US Army, mission specialist 2, 4th mission Previous missions: STS-57 (1993); STS-70 (1995); STS-88 (1998) LINNEHAN, Richard Michael, 44, civilian, mission specialist 3, 3rd mission Previous missions: STS-78 (1996); STS-90 (1998)

NEWMAN, James Hansen, 45, civilian, mission specialist 4, 4th mission Previous missions: STS-51 (1993); STS-69 (1995); STS-88 (1998) MASSIMINO, Michael James, 39, civilian, mission specialist 5

Flight Log

The scheduled launch on 28 February was postponed 24 hours before tanking operations commenced when adverse weather conditions threatened launch criteria. Waiting 24 hours also gave the launch team the option of back-to-back launch opportunities, but they did not need them as launch occurred without delay on 1 March. Following the launch, controllers noted a degradation of the flow rate in one of two freon coolant loops which help dissipate heat from the orbiter. After a management review, the mission was given a “go” for its full duration. The problem had no impact on the crew’s activities and the vehicle de-orbited nominally.

Hubble was grappled and secured in the payload bay by the RMS on 2 March (FD 2). A series of five EVAs were completed by the crew, working in pairs. Grunsfeld (EV1) and Linnehan (EV2) completed EVAs 1, 3 and 5, while Newman (EV3) and Massimino (EV4) completed EVAs 2 and 4. When not performing an EVA, the resting

STS-109

John Grunsfeld (right) and Richard Linnehan signal the close of the fifth and final EVA at Hubble. One more service mission is planned for the telescope in 2008

 

team also acted as IV crew for those who were outside, and serviced, cleaned and prepared their own equipment ready for their next excursion. Each EVA was supported by Nancy Currie operating the RMS, with Altman and Carey photo – documenting the activities.

During the first EVA (4 Mar for 7 hours 1 minute), the astronauts removed the older starboard solar array from the telescope (attached during STS-61 in December 1993) and installed a new third-generation array. The old (retracted) array was then stowed in Columbia’s payload bay for return to Earth for analysis of its condition after nine years in space. During EVA 2 (5 Mar for 7 hours 16 minutes), the new port array was installed, together with a new Reaction Wheel Assembly after the removal of the older array. The astronauts also installed thermal blankets on Bay 6, door stop extensions on Bay 5 and foot restraints to assist with the next EVA. EVA 2 also included a test of bolts located on the aft shroud doors. The lower two bolts were found to need replacing, which they accomplished successfully. EVA 3 (6 Mar for 6 hours 48 minutes) was delayed by a fault in Grunsfeld’s suit, but after changing the HUT, they continued with the EVA programme. This included replacing the Power Control Unit (PCU) with a new unit capable of handling 20 per cent of power output generated from the new arrays. The extracted PCU was the original launched on the telescope in 1990, and this operation required the telescope to be powered down. This was the first time since its launch that Hubble had been turned off. The astronauts removed all 36 connectors to the old PCU and stowed it in the payload bay before attaching the new unit within 90 minutes. One hour later, the new unit passed its tests and Hubble came back to life. EVA 4 (7 Mar for 7 hours 18 minutes) completed the first science instrument upgrade of the mission by removing the last original instrument on the telescope, the Faint Object Camera, and installing the Advanced Camera for Surveys. They also installed the first element of an environmental cooling system, called the Electronics Support Module (ESM). The rest of the system would be installed the following day. The final EVA (8 Mar for 7 hours 32 minutes) saw the installation of the Near Infrared Camera and Multi-Object Spectrometer (NICMOS) in the aft shroud and the connection of cables to the ESM. They also installed the Cooling System Radiator on the outside of Hubble and fed radiator wires through the bottom of the telescope to connections on NICMOS.

Hubble was released by the RMS on 9 March (FD 9) and the next day was a rest day for the astronauts. During the day, they took the opportunity to speak with the ISS-4 crew (Yuri Onufriyenko, Carl Walz and Dan Bursch). FD 11 saw a full systems check before landing at the first opportunity at the Cape on FD 12, rounding out a highly successful mission. At this time, there was a further Hubble service mission on the manifest (HST SM #4) in 2004 or 2005, with a close-out mission in 2010. The options of either bringing the telescope back to Earth for eventual display in a museum or leaving it in orbit, boosted to a higher apogee to reduce atmospheric drag, were still being considered when Columbia was lost in February 2003. It looked as though Hubble was likely be abandoned when its systems eventually failed, but there was also growing support both inside and outside of NASA to devote one Shuttle mission to revisit the telescope before the Shuttle fleet is retired in 2010. In

October 2006, a return to Hubble was authorised for 2008 due to public and scientific demand for keeping the telescope working for as long as possible.

Milestones

230th manned space flight

138th US manned space flight

108th Shuttle mission

27th flight of Columbia

52nd US and 85th flight with EVA operations

4th Hubble service mission (3B)

EVA duration record for single Shuttle mission (35hrs 55 min)

Int. Designation

2006-036A

Launched

9 September 2006

Launch Site

Pad 39B, Kennedy Space Center, Florida

Landed

21 September 2006

Landing Site

Runway 33, Shuttle Landing Facility, KSC, Florida

Launch Vehicle

OV-104 Atlantis/ET-118/SRB BI-127/SSME: #1 2044, #2 2048; #3 2047

Duration

11 days 19 hrs 7 min 24 sec

Call sign

Atlantis

Objective

ISS assembly mission 12A; delivery and installation of P3/P4 Truss

Flight Crew

JETT, Brent, 47, USN, commander, 4th mission

Previous missions: STS-72 (1996); STS-81 (1997); STS-97 (2000)

FERGUSON, Chris, 44, USN, pilot

TANNER, Joe, 56, civilian, mission specialist 1, 4th mission Previous missions: STS-66 (1994); STS-82 (1997); STS-97 (2000) BURBANK, Dan, 45, USCG, mission specialist 2, 2nd mission Previous mission: STS-106 (2000)

STEFANYSHYN-PIPER, Heidemarie, 43, USN, mission specialist 3 MACLEAN, Steve, 51, civilian, Canadian mission specialist 4

Flight Log

Set for a 29 August launch, the lift-off for the STS-115 mission to resume space station construction was postponed due to the proximity of tropical storm Ernesto. A decision was then made to roll back the STS-115 stack into the protection of the VAB for the duration of the storm as it passed KSC. This had a scheduling impact for the Russian launch of Soyuz TMA9 in September, but later the same day, NASA managers decided to reverse the decision and began moving the Shuttle back to the pad as weather predictions improved. On 6 September, a problem with Fuel Cell #1 in Atlantis was noted when a voltage spike in the coolant pump was recorded, threat­ening the planned 8 September launch. Analysis indicated that this was not a problem that would prevent the launch, but when a fuel cut-off sensor in the ET caused concern during the final minutes of the count, the mission was postponed 24 hours at the T — 9 minute mark. After a nominal performance during tests, the launch was given the all clear to proceed, which it did without further incident.

The delay had resulted in a short postponement of the launch of Soyuz TMA9 to the station and the shortening of the STS-115 mission by a day.

STS-115

Displaying a new set of wings, this photograph of ISS taken from the departing Shuttle reveals the newly-installed solar arrays delivered and installed by the crew of STS-115

The first day in orbit found the crew preparing equipment for the docking and EVA activities, as well as inspecting the thermal protection system on the orbiter. After analysis on the ground, no significant damage was found. Prior to docking on 11 September, the orbiter was flipped to allow the ISS-13 crew to observe and photo­document the TPS. Less than two hours after docking, the crew entered the station for the first time. At the end of the day, the first EVA crew of Tanner (EV1) and Stefanyshyn-Piper (EV2) “camped-out” for the night in the Quest airlock to purge their bloodstreams of nitrogen, which would shorten EVA preparations the next day. This pair completed the first and third EVAs of the mission, with Burbank (EV3) and Canadian Steve MacLean (EV4) completing the second EVA. All three EVAs (12 Sep for 6 hours 26 minutes; 13 Sep for 7 hours 11 minutes; and 15 Sep for 6 hours 42 minutes) were associated with the installation of the P3/P4 Truss and the deployment of the solar arrays and radiators.

No focused inspection of the Atlantis TPS was required after detailed analysis of the images from the crew, RMS and station inspections, so after the first two EVAs were completed, the crew rested for a couple of days and turned their attention to the transfer of logistics to and from the station. Such was the success of the first two EVAs, the crew managed to complete several get-ahead tasks along with their primary objectives.

On 17 September, Atlantis undocked from ISS after a visit lasting six days. Early the next morning, as the Shuttle began preparations for the return to Earth, Soyuz TMA9 was launched from Baikonur. With 12 space explorers in orbit at the same time

on three different vehicles (six astronauts on board Atlantis, three on Soyuz and three on ISS), it was the most people in space at the same time since April 2001, when the ISS-2, STS-100 and Soyuz TM32 crews (totalling 13 crew members) were all aloft. The hatches were open for 5 days 21 hours and 57 minutes and during this time, the two crews transferred 362.88 kg of hardware and 473 kg of water into the station and returned 491 kg of unwanted hardware and trash. In addition, 90.72 kg of launch lock restraints and unnecessary hardware was placed in Progress M56 for disposal.

Another inspection of the TPS of Atlantis was completed the day after undocking and the following day, the Shuttle crew spoke with both the crew on ISS and the crew on the approaching Soyuz TMA9 craft in a three-way link up. On 19 September the mission was extended in order to re-check some of the TPS areas of Atlantis after small unidentified particles were found floating near the Shuttle. There were sufficient supplies to allow the mission to be extended until 22 September or for them to return to ISS for a possible rescue mission if anything untoward been found. However, analysis revealed no significant problems and Atlantis was cleared for landing on 21 September (the previous day had been ruled out due to weather concerns). In the event all went well, and Atlantis made a textbook landing at night at the SLF at the Cape.

During homecoming events in Houston on 21 September, Stefanyshyn-Piper collapsed twice and had to be assisted by officials and crew members. She was not taken to hospital and the effects were attributed to her adjustment to gravity after her first 12-day flight into space.

Milestones

249th manned space flight

146th US manned space flight

116th Shuttle mission

27th flight of Atlantis

19th Shuttle ISS mission

7th Atlantis ISS mission

59th US and 98th flight with EVA operations

American orbital launchers

The Atlas ICBM was used to launch four manned Mercury missions in 1962-3, while the Titan II ICBM launched ten Gemini crews between 1965-6. A modified Titan II would have been used to fly the manned DynaSoar military space plane in the mid – 1960s, but this was cancelled in 1963 and replaced by the Gemini-based military Manned Orbital Laboratory. This was due to be launched on a Titan IIIM starting in 1966 but was also cancelled (in 1969), with some of its astronauts transferring to NASA.

The Atlas D intercontinental ballistic missile (ICBM) had a thrust of 166,470 kg (367,066 lb) from two Rocketdyne LR89 engines – which were burnt out and separated at about T + 2 min 14 sec – and an LR105 central sustainer engine. These were powered by liquid oxygen and kerosene. The Atlas was stabilised at lift-off by two powerful vernier engines. The Mercury-Atlas combination was 29 m (95 ft) high. The Atlas booster for the fifth manned mission was the first of a new model to be used for Mercury and was static test-fired on the pad because the US Air Force was concerned about turbo-pump failures that had occurred on some military ICBM launches. Atlas 113D would also ascend on ignition, rather than remaining on the pad for the previously prescribed two-second hold down period.

The Gemini Launch Vehicle (GLV) was a modified ICBM. Its twin first-stage LR-87 engines burned nitrogen tetroxide and hydrazine hypergolic propellants which ig­nited spontaneously on contact. The first-stage engines had a thrust of 195,046 kg (430,076 lb). The second stage, with a smaller LR-91 engine, had a thrust of 45,359 kg (100,017 lb). First-stage cut-off came at T + 2 min 30 sec, with a “fire in the hole’’ second-stage ignition following immediately. Orbit was achieved in 5 min 30 sec after launch. The launch vehicle was 3.04m (10 ft) in diameter and with Gemini on top, was 33.22m (109ft) tall.

The Saturn family of launch vehicles was developed for civilian space launches by a team led by Werner von Braun. The series built upon the successes and proven hardware of its early variants (Saturn 1 and 1B) before the huge Saturn V was used to send American astronauts to the Moon. Other variants were proposed but none were funded or built. Following a series of unmanned launches, the Saturn 1 manned missions were cancelled as unnecessary. After unmanned test flights, the Saturn 1B

American orbital launchers

Comparison of the US Mercury, Gemini and Apollo space capsules, and their launchers

launched one Apollo crew on a test flight in 1968, three Skylab space station crews in 1973-4 and the US part of the Apollo-Soyuz Test Program in 1975. Just two unmanned test flights were flown before the Saturn V carried a crew aloft for the first time. Apollo 8 and 10-17 launched their crews to the Moon in 1968-72, while Apollo 9 launched to Earth orbit as planned.

The Saturn 1B launch vehicle, with the launch escape system on top of the Command Module, was 74.37 m (244 ft) tall. The launch escape system comprised a 10m (33ft) high tower with a 66,675kg (147,018lb) thrust solid propellant motor, which could be used on the pad or during the first 100 seconds of launch. When ejected, it pulled away a conical blast shield from the Command Module, exposing the latter’s five windows. The first stage of the Saturn 1B comprised eight H1 engines, developing a thrust of 743,899 kg (1,640,297 lb) and burning the RP1 and liquid oxygen propellants for the first 150 seconds. The second stage was the S-IVB cryogenic liquid oxygen/ liquid hydrogen stage that would also form the third stage of the Saturn V booster. The S-IVB was powered by the J2,102,059 kg (225,040 lb) thrust engine with a burn time of 450 seconds. This engine could be restarted. The Saturn S-IVB also included the all­important Instrument Unit, the vehicle’s guidance and performance system. The

Saturn 1B was also the first manned launch vehicle used that was not a converted ballistic missile.

The Saturn V launch vehicle was 110.64 m (363 ft) high from the base of the F1 engines to the tip of the launch escape system tower. The first stage, called the S-1C, had five F1 engines developing a thrust of 3,442,801kg (7,591,376 lb) and burning liquid oxygen and RP1 propellants at a rate of 15 tonnes a second. The second stage, the S-11, also had five engines, called J2, with a thrust of 498,956kg (1,100,198 lb). The third stage was the S-IVB from the Saturn 1B launch vehicle. The whole vehicle weighed 2,903,020 kg (6,401,159 lb) at lift-off. The third stage was used for the Trans-Lunar Injection (TLI) burn to take the spacecraft out of Earth orbit and towards the Moon. The last Saturn V launch was a two-stage variant that carried the unmanned Saturn Workshop (Skylab) – itself a modified former S-IVB stage – in 1973. The earlier and larger Nova launch vehicle was abandoned in favour of the Saturn class of vehicles, which would be developed much quicker.

American orbital launchers

The Space Shuttle flew its first mission in 1981 and will be retired in 2010, although the programme may be extended if there are any further delays to the completion of the International Space Station. The “Space Shuttle” is a combination of boosters, fuel tank and orbital vehicle, often termed “the stack”. The orbiter is the manned portion of the vehicle and there have been six orbiters built: OV-101 (Enterprise) was used for

American orbital launchers

With the Solid Rocket Boosters lit, the Shuttle is committed to launch

atmospheric and ground tests; OV-102 (Columbia 1981-2003) was the first to launch to space and was lost in the STS-107 re-entry accident; OV-099 (Challenger 1983­1986) was a former structural test article and was lost in the STS 51-L launch accident; OV-103 (Discovery) is the oldest remaining vehicle and has been in service since 1984; OV-104 (Atlantis) has been used since 1985; and OV-105 (Endeavour) was built as a replacement for Challenger and was introduced in 1992.

The Space Shuttle orbiter Enterprise, which was to have been refurbished for space flight later, made five approach and landing atmospheric glide flights over Edwards Air Force Base in 1977, being air-launched from the back of a Boeing 747. Three flights were piloted by NASA astronauts Fred Haise and Gordon Fullerton and the other two by Joe Engle and Richard Truly. The longest glide flight, ALT 3, lasted 5 min 34 sec. Columbia was the first space flight-worthy orbiter and weighed 99,454 kg (219,296 lb) at orbital insertion. The orbiter measured 37.24 m (122 ft) long, with a wingspan of 23.79 m (78 ft). Three liquid hydrogen/liquid oxygen main engines, with a maximum thrust rating of 100 per cent, 170,098 kg (375,066 lb) each at sea level, took the orbiter into an initial orbit, which was then augmented by firing the Orbital Manoeuvring System (OMS) engines. These were powered by nitrogen tetroxide and UDMH, which also powered the reaction control thrusters. Power was provided by a liquid oxygen/ liquid hydrogen fuel cell system. A Thermal Protection System (TPS) heat shield tile system, comprising over 35,000 tiles, covered the orbiter to protect it from re-entry temperatures of between 370 and 1,260°C. A 756,453 kg (1,667,979lb), 47m (154 ft) long, 3.7 m (12 ft) wide External Tank (ET), painted white on the first two missions, held the SSME liquid oxygen and liquid hydrogen. Attached to it were two 45.46 m (149 ft) long, 3.7 m (12 ft) wide Solid Rocket Boosters (SRB), weighing 586,502 kg (1,293,237lb). Tail to nose, the Shuttle stack measured 56.144m (184ft) tall. The orbiter, an unpowered glider, had conventional flaps, rudder and ailerons for control in the atmosphere. Columbia’s STS-1 landing speed was 344kph (214mph). Improve­ments were made to the Shuttle fleet all the time. For example, Challenger was equipped with SRBs with an uprated thrust of 1,469,200 kg (3,239,586 lb) on its first mission, as well as main engines which were throttled up to 104 per cent for the first time. It also carried a new lighter weight external tank. Much of the areas covered with Low Temperature Surface Insulation tiles on Columbia were covered by lighter blankets of Advanced Flexible Reusable Surface Insulation on Challenger.

TO THE MOON

The space race ultimately turned into the Moon race after President Kennedy’s challenge in May 1961 for the USA to land a man on the Moon before the end of the decade. Human space exploration wasn’t going to involve step-by-step advances, but a crash programme.

Gemini

To cover the steps that still needed to be learned a new programme, Gemini, was devised. Now, the Americans could develop the technologies and experience required to go the Moon, including spacewalks, rendezvous and docking and long-duration flights. Ten crewed flights were launched between 1965 and 1966.

The distinctive black and white Gemini spacecraft consisted of two components; the re-entry module, of similar configuration but larger than Mercury, with a pres­surised cabin, re-entry control, and rendezvous and recovery sections; and the adapter module, with retro-rockets and equipment. Gemini 3 – which did not carry rendezvous systems – weighed 7,111 kg (15,680lb) and measured 5.58m (18ft) long with a base diameter of 2.28 m (7.5 ft). The re-entry module was 3.35m (11ft) long and 2.28 m (7.5 ft) at its heat shield base.

Gemini 3’s systems included a 100 per cent oxygen environmental control system, electrical batteries – fuel cells would be fitted for the first time on Gemini 5 – sixteen liquid-fuelled orbital attitude and manoeuvring system thrusters, and four solid propellant 1,133 kg (2,498 lb) thrust retro re-entry control system rockets. Gemini was also equipped with ejection seats and did not have a launch escape system. There was a drogue and one main parachute, and the landing sequence ended with Gemini moving from vertical to 30° horizontal position for splashdown.

MERCURY ATLAS 9

Подпись:1963-015A

15 May 1963

Pad 14, Cape Canaveral, Florida

16 May 1963

128 km southeast of Midway Island, Pacific Ocean Atlas 130D; spacecraft serial number SC-20 1 day 10 hrs 19 min 49 sec Faith 7

First US 24-hour space flight

Flight Crew

COOPER, Leroy Gordon Jr., 36, USAF, pilot

Flight Log

Such was the increased confidence in the Mercury spacecraft and manned space flight, that NASA not only planned a flight three times as long as Schirra’s, but also increased the duration again in November 1962 to a full 22 orbits. The man in the hot seat, Gordon Cooper, was named the same month, with a May 1963 launch date as the target. Cooper, who affirmed his faith in God, his country and the Mercury team by naming his spacecraft Faith 7, had a packed flight plan, with emphasis on photo­graphy. He called the mission, the “flying camera’’. The camera was fixed on to the tripod on 22 April and was ready to go on 14 May.

Unfortunately, the gantry tower refused to budge because water had seeped into its diesel fuel pump and when the gantry was moved away two hours later, radar data from the Bermuda tracking station was insufficient and the launch was scrubbed. Not so on 15 May, when the relaxed Cooper awoke from a catnap in Faith 7 in time to be launched at 08: 04 hrs local time. He reached his 32.5° orbit with an apogee of 267 km (166 miles) and a peak velocity of 28,238 kph (17,547 mph) five minutes later. Cooper remained extremely unruffled and calm throughout the flight, which featured the first in-flight television from a US spacecraft, although the pictures were disappointing.

Cooper’s photography from Faith 7, however, was a revelation, confirming to observers his own reports of being able to see the wakes of ships and smoke from a log cabin in the Himalayas with the naked eye. Cooper deployed a small flashing beacon from Faith 7, the first deployment in history, as well as a tethered balloon like Schirra’s. The flight went swimmingly, with Cooper becoming the first American to sleep in space, but during the nineteenth orbit, the astronaut noticed the one-G light coming on, which apparently detected the onset of gravity.

Tracing the cause, the astronaut discovered that the attitude and stabilisation control system a/c converter had failed. The astronaut would have to perform an

MERCURY ATLAS 9

Gordon Cooper heads for orbit aboard Mercury Atlas 9

entirely manual re-entry, which he did perfectly, splashing down just 7 km (4 miles) from the USS Kearsage, 128 km (80 miles) southeast of Midway Island in the Pacific Ocean, at T + 1 day 10 hours 19 minutes 49 seconds, the longest launch-to-landing solo US manned space flight in history. A planned three-day mission (Mercury-Atlas 10/Freedom II, flown by Alan Shepard) was mooted but scrapped, and the Mercury programme ended officially on 12 June 1963

Milestones

10th manned space flight

6th US manned space flight

6th and final Mercury manned flight

1st satellite deployment from manned spacecraft

VOSTOK 5

AND 6

Int. Designation

1963-020A (Vostok 5); 1963-023A (Vostok 6)

Launched

14 (Vostok 5) and 16 (Vostok 6) June 1963

Launch Site

Pad 1, Site 5, Baikonur Cosmodrome, Kazakhstan (both launches)

Landed

19 June 1963

Landing Site

619.4km northeast of Karaganda, Kazakhstan (Vostok 6); 539 km northwest of Karaganda, Kazakhstan (Vostok 5)

Launch Vehicle

R7 (8K72K); spacecraft serial number (11F63/3KA) #7 (Vostok 5); and #8 (Vostok 6)

Duration

4 days 23 hrs 6 min (Vostok 5); 2 days 22 hrs 50 min (Vostok 6)

Callsign

Yastreb (Hawk) – Vostok 5; Chaika (Seagull) – Vostok 6

Objective

Second group flight; five-day solo flight and first female space flight

Flight Crew

BYKOVSKY, Valeri Fyodorovich, 28, Soviet Air Force, pilot Vostok 5 TERESHKOVA, Valentina Vladimirovna, 26, Soviet Air Force, pilot Vostok 6

Flight Log

The much-rumoured launch of Vostok 5 was delayed by bad weather on 13 June but the following day, at 17:00 hrs local time at Baikonur, launch pad 1 reverberated to the sound of another SL-3 ignition as cosmonaut Valeri Bykovsky began what was planned as a long-duration mission. At 4 days 23 hours 6 minutes, it actually became (and still remains) the longest manned solo space flight in history. Vostok 5 entered a 65° inclination orbit with an apogee of 209 km (130 miles) as rumours persisted that another Vostok would be launched the following day. It was to be a Vostok that would overshadow Bykovsky’s feat.

Vostok 6 carried the first woman (and tenth human) to venture into space. Valentina Tereshkova was launched at 14: 30 hrs Baikonur time. Reflecting the frenetic space activity of the 1960s, in between the Vostok 5 and 6 launches, the USA had performed six satellite launches, all from California. Vostok 6 entered a 65° inclination orbit with a peak altitude of 218 km (135 miles) and almost immediately came to within 5 km (3 miles) of Vostok 5 for a brief encounter, which according to the western press went much further, with such headlines as “Valya chases her space date’’.

As Tereshkova was not a pilot, it was perhaps inevitable that she reportedly had difficulties in adapting to weightlessness, but the rumours of her being so ill that she pleaded to come home seem far-fetched, as it appears that the flight, originally

MERCURY ATLAS 9

Tereshkova and Korolyov in discussion prior to her historic space flight

planned to be a 24-hour affair, was in fact extended. The launch of a woman into space was undoubtedly a major propaganda coup for Premier Khrushchev, who may have ordered such a mission, a theory supported by the fact that the next woman to fly into space was not launched until 1982.

Tereshkova was the first of the space pair to land, 624 km (388 miles) northeast of Karaganda at mission elapsed time of 2 days 22 hours 50 minutes. As the landing was a nominal one, she is thus the only woman to end a space flight outside her spacecraft, as well as the only one to make a solo female space flight. Bykovsky was the third Vostok pilot to experience a partial separation of the descent module but the sepa­ration occurred prior to the worst part of the re-entry profile and he returned to Earth about 540 km (336 miles) northwest of Karaganda. Plans were set in motion for a Vostok 7 mission lasting a week, by “non-cosmonaut” doctor Boris Yegorov, in the summer of 1964 but, like the US Mercury programme, the Soviet Vostok project ended after six flights. However, the next series of spacecraft (Soyuz, or “Union”) would not be ready for some time and so in order to appear ahead in the space race with the Americans, the Vostok was converted into what seemed to outsiders to be a radically new and improved spacecraft – Voskhod.

Milestones

11th and 12th manned space flights 5th and 6th Soviet manned space flights

5th and 6th Vostok manned flights

1st space flight with female crew (Vostok 6)

1st joint male-female space flight

Bykovsky has held the solo space flight record for over 43 years

On 27 June 1963, Robert Rushworth, 39, of the USAF flew X-15-3 on the third astro – flight, to 88 km. Less than a month later, on 19 July 1963, Joe Walker, 42, flew the same vehicle on the fourth astro-flight, this time to 105 km. Finally this year, on 22 August 1963, Walker flew X-15-3 to 107 km in the fifth astro-flight, the highest altitude any X-15 would attain.

Подпись:

Подпись: VOSKHOD 1
Подпись: 1964-065A 12 October 1964 Pad 1, Site 5, Baikonur Cosmodrome, Kazakhstan 13 October 1964 3,105 km northeast of Kustanai R7 (11A57); spacecraft serial number (11F63/3KV) #3 1 day 17 min 3 sec Rubin (Ruby) Multi-crew flight

Flight Crew

KOMAROV, Vladimir Mikhailovich, 37, Soviet Air Force, commander FEOKTISTOV, Konstantin Petrovich, 38, civilian, flight engineer YEGOROV, Boris Borisovich, 27, civilian, doctor

Flight Log

Voskhod (“Sunrise”) 1 provided the classic illustration of how the secret Soviet space programme completely misled the west. After the Vostok missions, Sergei Korolyov, the then anonymous space designer, considered improvements to the basic spacecraft to allow longer missions by more than one passenger. These studies led to the design of a new spacecraft, Soyuz, which would perform Earth orbital and lunar looping missions and support a possible lunar landing programme. Delays to Soyuz meant that there would be a hiatus in the manned space programme, to which Premier Khrushchev reacted in customary fashion, demanding a multi-crewed space flight before the United States launched its two-man Gemini spacecraft in early 1965.

As Soyuz could not be accelerated, Korolyov responded with a version of the uprated Vostok. But in order to launch three men rather than two, as the Americans were planning, practically all the “stuffing” had to be taken out of Vostok and the crew would have to fly without spacesuits and without any means of emergency escape. Voskhod would, however, carry a back up retro-rocket. Despite the imperfec­tions of Voskhod, seven cosmonauts seemed happy to be assigned to train for the most risky manned space flight in history. The three to be chosen were a commander, Vladimir Komarov, a scientist, Konstantin Feoktistov – who, it turned out, was the man who helped design Vostok to fly with three passengers – and a doctor, Boris Yegorov.

They arrived at the launch pad wearing cotton overalls and leather flying helmets, about to board the first SL-4 booster to fly a manned crew a few days after the one and only “test flight” of the “new” Voskhod, as Cosmos 47. Launch came at 12: 30hrs Baikonur time and soon after the spacecraft had reached its 65°, 409 km (254 miles)

MERCURY ATLAS 9

The first “space crew” walk down the red carpet to report on the success of their mission to welcoming officials in Moscow. L to r Feoktistov, Komarov, Yegorov

maximum altitude orbit, the western media went wild, reporting that Russia had launched a “mammoth” new spaceship in which the scientist and doctor would perform experiments while the commander controlled the mission. In truth, the conditions were so cramped inside the Voskhod that it must have been hard to eat and go to the toilet, let alone perform experiments, although Yegorov apparently performed some basic medical checks.

Khrushchev had the propaganda success he wanted, but as he was congratulating the crew by telephone, the receiver was taken from his hands. The Brezhnev-Kosygin takeover had begun and it was they who greeted the fortunate cosmonauts after they had landed safely. The crew remained in the spherical capsule as small retro – rockets fired just before touchdown to cushion the impact, some 310 km (193 miles) northeast of Kustanai. The mission lasted just 1 day 17 minutes 3 seconds, the shortest three-crew flight in history. The three-man crew apparently requested an extension but were refused by Korolyov, who quoted Shakespeare: “There are more things in heaven and Earth, Horatio…” At the time, no one knew the name of the chief designer, who had one more spacecraft to design before he succumbed to ill health in January 1966.

Milestones

13th manned space flight

7th Soviet manned space flight

7th Vostok manned flight

1st Voskhod manned variant flight

1st three-person crew

1st flight by crew without spacesuits

1st flight with no launch escape or ejection system

1st Soviet space flight to end with crew inside spacecraft

1st space flight with non-pilot, civilian crew

1965-022A

18 Подпись: Int. Designation Launched Launch Site Landed Landing Site Launch Vehicle Duration Callsign ObjectiveMarch 1965

Baikonur Cosmodrome, Kazakhstan

19 March 1965

180 km northeast of Perm, Siberia

R7 (11A57); spacecraft serial number (11F63/3KD) #4

1 day 2hrs 2 min 17 sec

Almaz (Diamond)

First Extra-Vehicular Activity (EVA – spacewalk) demonstration

Flight Crew

BELYAYEV, Pavel Ivanovich, 39, Soviet Air Force, commander LEONOV, Alexei Arkhipovich, 30, Soviet Air Force, pilot

Flight Log

The second of a planned series of multi-crew Voskhod missions got underway at 12: 00 Baikonur time, entering a 65° inclination orbit with the highest manned apogee to date of 495 km (308 miles). Instead of three crewmen without spacesuits, there were two, this time suitably attired. This Voskhod had been reconfigured to carry a telescopic airlock leading from the crew cabin. The space where the third seat had been was left free to give one of the crewmen, Alexei Leonov, the room in which to don an emergency oxygen backpack and connect an umbilical air and communications tether to his spacesuit, before crawling through the airlock after the spacecraft had been depressurised.

The first walk into open space began at the start of the second orbit of Voskhod, as Leonov emerged from the airlock at the end of his 5 m (16 ft) tether, watched by two television and film cameras attached to the end of the airlock and on top of the back­up retro-rocket. Leonov cavorted in space doing cartwheels, not for show but because he was essentially out of control as his umbilical snaked around. His official free spacewalk lasted 12 minutes 9 seconds, but he was in the vacuum environment for about 20 minutes, since he couldn’t get back into the airlock. His spacesuit had ballooned more than anticipated and he had to squeeze himself back into the airlock quite forcibly before closing the hatch and re-pressurising the spacecraft.

Unfortunately, he forgot to retrieve the film camera which would have shown clear photos of the EVA rather than the blurred and fuzzy television reproductions. Nonetheless, Leonov’s exploits had a dramatic effect on the watching world, cap­turing more headlines than Gagarin himself, and this mission was one of the highlights of the “Space Age’’ of the 1960s. The rest of the flight went quietly until they

MERCURY ATLAS 9

The first “walk” in space

attempted retro-fire at the end of the seventeenth orbit. The prime retro-rocket in the instrument module of Voskhod failed to fire because of a sensor attitude control malfunction.

The cosmonauts made one more orbit as, not without a certain amount of drama, preparations were made to fire the back-up retro-pack on the next pass. The instru­ment section was apparently jettisoned (again not cleanly) before this, and the Voskhod spherical flight cabin was manually orientated by Belyayev, who punched the retro-pack arming device. The re-entry was quite dramatic and the capsule natur­ally missed the main recovery area by 960 km (597 miles), landing in the thick, snow – covered forest near the city of Perm. A damaged telemetry antenna made it impossible for the rescue teams to locate the craft, so the cosmonauts put their emergency landing training into effect, lighting a fire and waiting for rescue. However, ravenous wolves compelled their return to the capsule and it was two and a half hours before a helicopter spotted the capsule, thanks to the parachutes which were splayed out across the tree tops. Ground vehicles rescued the crew after they had spent a night in the forest.

Observers in the west, expecting a landing announcement to be made at the end of the seventeenth orbit, suspected that something was wrong and were only told of the touchdown when the crew had been located, four hours later. The drama of

the landing events was only fully revealed a year later, rather perversely, after the emergency US landing of Gemini 8. Flight time was 1 day 2 hours 2 minutes 17 sec­onds. This proved to be the last Voskhod manned mission. There had originally been plans for a series of at least seven manned Voskhod flights. Voskhod 3 was to have been a two-man 15-20-day extended scientific mission, and then Voskhod 4 would have flown a 15-day biomedical mission with a cosmonaut doctor in the crew. Voskhod 5 would be an all female crew with an EVA, Voskhod 6 was a 14-day EVA mission featuring the use of a small manoeuvring unit, and Voskhod 7 would attempt tether dynamics with the spent upper stage before flying a 10-15 day mission. There was also a plan to include a professional Soviet journalist on board a Voskhod but all these flights were cancelled.

Milestones

14th manned space flight

8th Soviet manned space flight

8th Vostok manned flight

2nd Voskhod manned variant flight

1st manned space flight with two crew

1st space flight with EVA operations

1st extended mission

Подпись:

Подпись: GEMINI 3
Подпись: 1965-024A 23 March 1965 Pad 19, Cape Kennedy, Florida 23 March 1965 Western Atlantic Ocean Titan II Gemini Launch Vehicle-3 (GLV-3); spacecraft serial number 3 4hrs 52 min 51 sec Molly Brown/Gemini Three Three-orbit manned test flight; test of orbital manoeuvring system

Flight Crew

GRISSOM, Virgil Ivan “Gus”, 39, USAF, commander, 2nd mission Previous mission: Mercury-Redstone 4 (1961)

YOUNG, John Watts, 35, USN, pilot

Flight Log

Project Gemini was born as the logical follow-on to the Mercury programme, but its raison d’itre was changed by President Kennedy’s pledge to land a man on the Moon before 1970. Gemini was to act as the testing ground for all the manoeuvres and operations to be performed on an Apollo mission, but in Earth orbit – orbital manoeuvring, rendezvous, docking, extended flights and spacewalking. The task of Gemini 3 was straightforward: with the aid of the first computer on a manned spacecraft, Gemini 3 would change its orbit.

The crew was chosen at the time of the Gemini 1 unmanned test flight and was well into training by the time unmanned Gemini 2 had become the first to be recovered. Command pilot Gus Grissom and his pilot John Young, the Taciturn Twins as they were dubbed, were overshadowed by the exploits of Voskhod 2 five days earlier, particularly as Gemini 3 was to make only a modest three orbits. The crew were lying in their ejector seats inside Gemini 3 at 07: 30 hrs, waiting for a 09: 00 hrs launch. At T — 35 minutes, the Titan II first-stage oxidiser line sprang a leak and a handy wrench was required, delaying the launch by 24 minutes. The hypergolic engines of the Titan gave out a high-pitched whine and sprang to life and the mission lifted off.

As the second stage ignited while still attached to the first stage, its exhaust spewing out of the lattice framework between the two, the rocket was surrounded by a bright aurora, disconcerting the pilot. After reaching the 32.5°, 224km (139 miles) peak apogee orbit, the crew was immediately assigned to a series of science

MERCURY ATLAS 9

Young (left) and Grissom aboard Gemini 3

experiments, including a sea urchin cell growth experiment, which failed because Grissom was rather heavy-handed with it.

At last, the frustrated astronauts had some real space flying to do as, at T + 1 hour 30 minutes, Grissom performed the first orbital manoeuvring system burn, for 75 seconds. Two more burns followed, with the last placing Gemini 3’s perigee at 72 km (45 miles), low enough to ensure re-entry even if the retros failed to fire, which they didn’t. Grissom tried to use Gemini’s lift capability to reduce a predicted landing miss but the capability of the spacecraft was less than anticipated and resulted in a 111 km (69 miles) miss. As Gemini assumed splashdown position, it literally yanked from vertical to an almost horizontal position, pitching the crew forward and smashing Grissom’s faceplate against the instrument panel.

The flight ended near Grand Turk Island in the Atlantic Ocean at T + 4 hours 52 minutes 51 seconds, the shortest US two-crew mission. The landing miss meant a long wait in heaving seas but Grissom – remembering Liberty Bell – elected to stay on board with the hatch well and truly closed. Grissom lost his pre-launch breakfast and both doffed their spacesuits in the heat. They later walked rather ignominiously along the deck of the carrier Intrepid, to which they had been helicoptered, in sporting underwear beneath bathrobes. After the Liberty Bell 7 incident, Grissom named his next space craft “Molly Brown’’ after the hit Broadway show “The Unsinkable Molly

Brown”. NASA was not happy about this and asked him to change the name, but when he indicated that his second choice was “Titanic” they relented. “Molly Brown” became the last named American spacecraft until Apollo 9 in March 1969.

Gemini 3 became known as the “corned beef sandwich flight”, when afterwards it was revealed that Young had been reprimanded for carrying food aboard and offering it to Grissom who, on taking a hefty bite, spread crumbs around the cabin. The prank was, not surprisingly, hatched by the back-up command pilot, Wally Schirra, who put the sandwich into Young’s spacesuit, but the joke got out of hand and became the subject of a Congressional inquiry. The cost of the sandwich, which Schirra had bought in Cocoa Beach, escalated, and it became known as the “$30 million sandwich’’.

Milestones

15th manned space flight 7th US manned space flight 1st Gemini manned flight

1st manned space flight to perform orbital manoeuvres

1st US two-man crew mission

1st flight by crewman on second mission

Int. Designation

1981-111A

Launched

12 November 1981

Launch Site

Pad 39A, Kennedy Space Center, Florida

Landed

14 November 1981

Landing Site

Runway 23, Edwards Air Force Base, California

Launch Vehicle

OV-102 Columbia/ET-3/SRB A09; A10/SSME #1 2007; #2 2006; #3 2005

Duration

2 days 6 hrs 13 min 13 sec

Callsign

Columbia

Objective

Second Orbital Test Flight (OFT-2); tests of the Remote Manipulator System (RMS)

Flight Crew

ENGLE, Joseph Henry, 49, USAF, commander TRULY, Richard Harrison, 44, USN, pilot

Flight Log

As Columbia was being prepared for its second mission, originally scheduled for 10 September then pushed to 30 September, with 1,000 new tiles, new RCS com­ponents, an OMS nozzle and fuel cells, nitrogen tetroxide leaked from a ruptured fuel line during propellant loading, damaging another 240 tiles on its nose. The launch was postponed to 4 November. Things looked good but the launch was delayed for 2 hours 40 minutes and finally scrubbed, holding at T — 31 seconds, when an oil flush on one of the APUs failed and a computer malfunctioned. Both had to be replaced before a new launch attempt, eight days later.

The first flight of a re-used manned spacecraft began at 10: 10 hrs local time and astronauts Joe Engle and Richard Truly (marking a space first by being launched on his birthday) were at last on their way, into a 38° inclination orbit which would have a maximum altitude of 219 km (136 miles). A five day flight was on the agenda, with a complement of science experiments and the testing of the Remote Manipulator System robot arm, being carried for the first time. An increase in the alkaline level of the electrolyte in one of Columbia’s three fuel cells spoiled the day for Engle and Truly, who were told to cram five days work into two, as mission rules dictated.

The RMS did not work quite as well as planned since it suffered a back-up drive failure, but TV cameras at its end gave interesting views of the payload bay and other parts of the Shuttle. Engle did not get the chance to try out the Shuttle EVA suit inside the airlock. Mission scientists were pleased with the results from the science experi­ments, particularly the multi-spectral imaging radiometer and the Shuttle Imaging Radar. Columbia came home on the dry lake bed runway 23 at Edwards Air Force

STS-2

The launch of STS-2 sees Columbia become the first manned spacecraft to return to orbit

Base, touching down at a speed of 361 kph (224 mph), at T + 2 days 6 hours 13 minutes 13 seconds, main gear touchdown time.

Milestones

82nd manned space flight

33rd US manned space flight

2nd Shuttle flight

2nd flight of Columbia

1st manned space flight by reused spacecraft

Truly celebrates his 44th birthday by being launched into space (12 November)

Int. Designation

1985-043A

Launched

6 June 1985

Launch Site

Pad 1, Site 5, Baikonur Cosmodrome, Kazakhstan

Landed

26 September 1985

Landing Site

220 km northeast of Dzhezkazgan

Launch Vehicle

R7 ( 11A511U2) spacecraft serial number (7K-ST) # 19L

Duration

112 days 3hrs 12min 6 sec (Dzhanibekov)

168 days 3 hrs 51 min 0 sec (Savinykh – returned in Soyuz T14)

Callsign

Pamir (Pamirs)

Objective

Salyut 7 rescue and recovery mission

Flight Crew

DZHANIBEKOV, Vladimir Aleksandrovich, 43, Soviet Air Force, commander, 5th mission

Previous missions: Soyuz 27 (1978); Soyuz 39 (1981); Soyuz T6 (1982); Soyuz T12 (1984)

SAVINYKH, Viktor Petrovich, 43, civilian, flight engineer, 2nd mission Previous mission: Soyuz T4 (1981)

Flight Log

After the return of the long-duration Soyuz T10 trio from the Salyut 7 space station in late 1984, another three manned missions were planned for 1985/1986 to continue manned operations. Indeed, the crews had been selected and were in training. Soyuz T13 would be launched in May, crewed by Vladimir Vasyutin, Viktor Savinykh and Aleksandr Volkov to complete a six-month mission. They would be visited by Soyuz T14, carrying an all-female crew on a two-week mission in November. This crew would comprise commander Svetlana Savitskaya on her third mission, along with Yekaterina Ivanova and Yelena Dobrokvashina. The Soyuz T15 flight would then launch at the end of 1985 to complete the Salyut 7 programme by the spring of 1986, when a new station would have been launched. Soyuz T15 was to have been crewed by Viktor Viktorenko, Alexandr Alexandrov and Yevgeny Salei.

Then, in early 1985, came the blow that Salyut 7 was effectively dead in space. Contact had been lost and the space station was out of control. Systems were freezing and observers expected that it would never be manned again. There was concern that it would make a Skylab-like uncontrolled re-entry. It was decided to send the most qualified veteran cosmonaut (Vladimir Dzhanibekov, with four previous space flights to his credit) to the station along with veteran Salyut 6 FE Savinykh to see if they could restore the station to operational use. Dzhanibekov had already proven his

SOYUZ T13

Savinykh and Dzhanibekov wearing thermals during the early occupation of the stricken space station

docking skills in past missions, and all his knowledge would be required on this demanding space flight. If the two men could restore the station sufficiently, then the Soyuz T14 crew would be sent to Salyut to resume their intended programme. Flying along with the T14 crew would be Salyut veteran Georgi Grechko, on a short science – orientated mission. He would return with Dzhanibekov after a few days on the Salyut.

The fate of the other crews would be decided if Salyut could be restored. The launch of Soyuz T13 at 12:40 hrs local time from Baikonur on 6 June to conduct “joint work” with Salyut 7 caught western observers by surprise. The two cosmonauts, Vladimir Dzhanibekov – the first Soviet to make five space flights – and flight engineer Viktor Savinykh, proceeded to fly one of the bravest and most remarkable space missions ever.

Soyuz T13 arrived at Salyut two days later, flying all around to check the condition of the exterior and finally docking at the front port with the aid of a new laser ranging device. The crew donned oxygen masks and lots of woolly clothing and entered the freezing space station. Salyut was stabilised so that its solar panels were pointing at the Sun for long enough periods to re-start some form of electrical power. The station’s life support system was fixed thanks to expert repairs by the two crewmen, who often retreated to Soyuz to warm their bodies. Communications directly from the station were restored and by late June, Salyut 7 was declared to be in an operational state.

Progress 24 arrived on 23 June with additional repair and replenishment supplies, and the crew even got to work on some experiments dedicated to Earth observation, while Progress loaded the Salyut propulsion system with fuel. Confounding experts who regarded the Soyuz T13 mission as finished, the Soviets launched a Heavy Cosmos module, rather than the Progress-class spacecraft that it was first suspected to be by analysts. Designated Cosmos 1669, it docked with Salyut on 21 July, enabling even more fruitful work to be conducted by the remarkable crew, which even went on EVA on 2 August to place two small solar arrays on the third large array on Salyut. The walk lasted about 5 hours.

Cosmos 1669 undocked on 28 August, making a controlled re-entry two days later, and the T13 crew went on conducting a mission as ordinary and routine as a normal residency. The 51.6° mission reached a maximum altitude of 359 km (223 miles). Soyuz T14 was launched and joined them on 18 September. Dzhanibekov and one of the T14 crew, the burly Georgy Grechko, undocked on 25 September, flew a day’s autonomous mission and came home – the first individual space travellers who were launched separately but landed together – at T13 flight time of T + 112 days 3 hours 12 minutes. Savinykh, meanwhile, remained on board Salyut 7 to attempt the longest manned space flight in history, only to be thwarted by his new commander’s illness.

Milestones

106th manned space flight

58th Soviet manned space flight

51st Soyuz mission

12th Soyuz T mission

1st reactivation of a dead space station

10th Soviet and 31st flight with EVA activities

Int. Designation

1990-019A

Launched

28 February 1990

Launch Site

Pad 39A, Kennedy Space Center, Florida

Landed

4 March 1990

Landing Site

Runway 23, Edwards Air Force Base, California

Launch Vehicle

OV-104 Atlantis/ET-33/SRB BI-036/SSME #1 2019;

#2 2030; #3 2027

Duration

4 days 10 hrs 18 min 22 sec

Callsign

Atlantis

Objective

6th classified DoD shuttle mission

Flight Crew

CREIGHTON, John Oliver, 45, USN, commander, 2nd mission Previous mission: STS 51-G (1985)

CASPER, John Howard, 46, USAF, pilot

MULLANE, Richard Michael, 45, USAF, mission specialist 1, 3rd mission Previous missions: STS 41-D (1984); STS-27 (1988)

HILMERS, David Carl, 40, USMC, mission specialist 2, 3rd mission Previous missions: STS 51-J (1985); STS-26 (1988)

THUOT, Pierre Joseph, 34, civilian, mission specialist 3

Flight Log

This DoD classified military mission by the orbiter Atlantis was always going to be a quiet affair, other than the usual comical revelation of exactly what the classified payload was going to be. In this case, it was a digital imaging and electronic signals intelligence satellite, which was to be deployed on the Shuttle’s eighteenth orbit, comparatively late in the proposed four-day mission, by a new system called the Stabilised Payload Deployment System, SPDS. This was fixed to the payload in the payload bay before launch and was to be used to rotate the satellite clear of the Shuttle before release by spring-loaded pistons.

Another innovation for the mission was its high inclination of 62°, ostensibly 5° over the safety limits for launches from the Kennedy Space Center, but on a trajectory which would not quite take it over land. As if to veil this fact as much as possible, Atlantis was first scheduled for a night launch on 16 February, which was eventually moved to 22 February, at 01: 00hrs local time. Before the crew could board the Shuttle, however, the weather caused concern and for the first time since Apollo 9, a US mission was delayed by the illness of the crew. In this case, it was commander John Creighton, who was suffering from an upper respiratory tract infection.

STS-36

Commander Creighton photographs views out of the overhead windows of Atlantis

His illness delayed the launch until 25 February and the count reached T — 31 seconds when a range safety computer went on the blink. By the time it had been fixed, the liquid oxygen was too cold for the SSMEs. The launch was cancelled the following day due to winds at altitude and a low cloud deck and was routinely postponed for 48 hours. On 28 February, the weather looked to win again, but with just seconds of the launch window remaining, Atlantis lit up the night sky at 02: 50 hrs local time, heading for its unique launch azimuth. Deployment of the classified satellite took place as planned and the mission ended quietly with a landing at Edwards Air Force Base at T + 4 days 10 hours 18 minutes 22 seconds.

It was revealed later that the satellite had apparently broken apart in orbit and two of the six resulting fragments had re-entered soon after. The satellite may have failed to fire its rocket stage to reach operational orbit. All in all, it seems that STS-36 was an expensive waste of a mission.

Milestones

132nd manned space flight 64th US manned space flight 34th Shuttle flight 6th flight of Atlantis

Int. Designation

1992-026A

Launched

7 May 1992

Launch Site

Pad 39B, Kennedy Space Center, Florida

Landed

16 May 1992

Landing Site

Runway 22, Edwards AFB, California

Launch Vehicle

OV-105 Endeavour/ET-43/SRB BI-050/SSME #1 2030; #2 2015; #3 2017

Duration

8 days 21 hrs 17 min 38 sec

Call sign

Endeavour

Objective

Capture, repair and redeployment of stranded satellite INTELSAT VI (F-3); Assembly of Space Station by EVA Methods demonstration (ASSEM)

Flight Crew

BRANDENSTEIN, Daniel Charles, 49, USN, commander, 4th mission Previous missions: STS-8 (1983); STS 51-G (1985); STS-32 (1990)

CHILTON, Kevin Patrick, 36, USAF, pilot

HIEB, Richard James, 36, civilian, mission specialist 1, 2nd mission Previous mission: STS-39 (1991)

MELNICK, Bruce Edward, 42, US Coast Guard, mission specialist 2,

2nd mission

Previous mission: STS-41 (1990)

THUOT, Pierre Joseph, 36, mission specialist 3, 2nd mission Previous mission: STS-36 (1990)

THORNTON, Kathryn Cordell Ryan, 39, civilian, mission specialist 4, EV3, 2nd mission

Previous mission: STS-33 (1989)

AKERS, Thomas Dale, 40, USAF, mission specialist 5, 2nd mission Previous mission: STS-41 (1990)

Flight Log

The maiden flight of the Endeavour (the replacement orbiter for Challenger which was lost in the 1986 launch accident) was an impressive mission that clearly demonstrated the value of having astronauts on board to overcome technical problems. Whether there was a need for Endeavour itself was a question long debated, but it was the loss of Challenger that finally secured the construction of the new vehicle from the structural spares that had been factored into the orbiter construction programme several years before. There was no such contingency to replace Columbia seventeen years later.

STS-49

Three astronauts hold onto the 4.5-ton Intelsat VI satellite after completing a six-handed “capture”. L to r are astronauts Hieb, Akers and Thuot, who stands on the end of the RMS. This first three-person EVA was the third attempt at grappling the satellite

Following the 6 April 1992 flight readiness firing of Endeavour’s three main engines, the management team decided to replace all three due to irregularities that had arisen in two of the high-pressure oxidiser turbo-pumps. The launch of STS-49 was set for 4 May, but was rescheduled for 7 May, with an early launch window that would offer better lighting conditions for photo-documentation of the behaviour of the new vehicle during its first ascent. The lift-off on 7 May was delayed by 34 minutes due to bad weather at the transoceanic abort landing site, as well as technical problems with one of Endeavour’s master event controllers.

The primary objective of the flight was the capture and redeployment of the Intelsat VI satellite that had been launched aboard a Titan rocket on 14 March 1990.

During the launch, the second stage of the Titan had not separated, preventing the satellite’s ascent into a geosynchronous orbit. Quick thinking by ground controllers triggered the separation of the satellite from the unused Perigee Kick Motor (PKM) that was still attached to the Titan stage, and careful use of onboard liquid propellant allowed the satellite to reach a thermally stable 299 x 309 nautical mile orbit. Sub­sequent data analysis suggested it would be more cost-effective to bring a new kick motor up to the stranded satellite on the Shuttle than to return it to the ground and relaunch it. The Hughes Aircraft Company’s Space and Communications Group worked with NASA to construct special hardware to support the EVA operations that would be required.

The crew split into two EVA teams. Thuot (EV1) and Hieb (EV2) were termed the Intelsat EVA crew for the satellite retrieval and redeployment, while Thornton (EV3) and Akers (EV4) would work on the planned evaluation of space station construction techniques. A specially designed capture bar would be used to capture the satellite but in the event, this did not work as planned. During the first attempt on 10 May, Thuot had been unable to attach the capture bar, causing the satellite to bounce away and tumble at even greater rates the more he tried. The following day, the rotation of the satellite had slowed sufficiently for Thuot to gently move the bar into place. This time, however, the latches on the bar failed to fire, causing the satellite to drift off once again. It became evident that the planned method of capture would not work and during 11 May, as the crew rested, plans were formulated for another attempt. This would be the last chance, as Endeavour had only enough propellant aboard to support one more rendezvous. The following day, the crew practised getting three pressure – suited astronauts into an airlock that was designed to accommodate just two. Other astronauts simulated the operation in the water tank at JSC and the crew played an important role in the final decision to try the first three-person EVA.

On 13 March, Thuot, Hieb and Akers ventured outside and placed themselves in foot restraints 120° apart around the payload bay. Hieb was stationed on the starboard wall of the bay and Akers stood on a borrowed strut from the ASSEM experiment, while Thuot rode the RMS. Brandenstein and Chilton flew Endeavour and gently closed in on the satellite, allowing all three EVA astronauts to reach up and grasp the satellite by the three electric motors that would deploy the satellite’s cylindrical solar panel. Over a difficult 85 minutes, the capture bar was finally attached to the satellite, allowing the RMS to manipulate it over the payload bay and onto the new kick motor. Thuot and Hieb then used hand-operated ratchets to pull the satellite down and latch it into place with four clamps. They then connected two electrical umbilicals. With the astronauts back in the airlock, but with an open hatch in case they were still required, the new PKM was ejected from the payload bay. Thirteen minutes later, a procedural error on the checklist prevented the initial deployment. The EVA set a new duration record, surpassing that of the Apollo 17 astronauts on the Moon in December 1972. The new engine worked perfectly on 14 May, placing the satellite on its way to geosynchronous orbit.

The same day, Thornton and Akers were in the payload bay performing the ASSEM EVA demonstration. Originally scheduled for two EVAs, the Intelsat diffi­culty had curtailed this to a single excursion. The pair assembled a pyramid out of struts to simulate a station truss section, then attached a triangular pallet to this to simulate the mass of a major component such as a propulsion module. Scheduled for three hours, the astronauts found that it took twice as long as expected and proved very tiring, forcing other activities planned for this EVA to be cancelled. The mission had been extended by two days to complete its primary objectives and this took a toll on the crew. They also had to complete the rest of their experiment programme, including the Commercial Proton Crystal Growth experiment, the UV Plume Instru­ment experiment and the USAF Maui Optical Site experiment. Post-flight inspections revealed negligible damage and the crew and flight controllers reported only minor problems. The new vehicle had joined the fleet in style.

Milestones

150th manned space flight 77th US manned space flight 47th Shuttle mission 1st flight of Endeavour

25th US and 46th flight with EVA operations 1st Shuttle mission to feature four EVAs 1st use of landing drag parachute 1st three-person EVA

1st astronaut attachment of rocket motor to orbiting satellite

Int. Designation

1994-006A

Launched

3 February 1994

Launch Site

Pad 39A, Kennedy Space Center, Florida

Landed

11 February 1994

Landing Site

Runway 15, Shuttle Landing Facility, Kennedy Space Center, Florida

Launch Vehicle

OV-103 Discovery/ET-61/SRB BI-062/SSME #1 2012; #2 2034; #3 2032

Duration

8 days 7 hrs 9 min 22 sec

Call sign

Discovery

Objective

Wake Shield Facility 1 operations; SpaceHab 2; first flight of a Russian cosmonaut on a US mission

Flight Crew

BOLDEN Jr., Charles Frank, 47, USMC, commander, 4th mission Previous missions: STS 61-C (1986); STS-31 (1990); STS-45 (1992) REIGHTLER Jr., Kenneth Stanley, 42, USN, pilot, 2nd mission Previous mission: STS-48 (1991)

DAVIS, Nancy Jan, 40, civilian, mission specialist 1, 2nd mission Previous mission: STS-47 (1991)

SEGA, Ronald Michael, 41, civilian, mission specialist 2

CHANG-DIAZ, Franklin Ramon, 43, civilian, mission specialist 3, 4th mission

Previous missions: STS 61-C (1986); STS-34 (1989); STS-46 (1992)

KRIKALEV, Sergei Konstaninovich, 35, civilian, Russian mission specialist 4, 3rd mission

Previous missions: Soyuz TM7 (1988); Soyuz TM12 (1991)

Flight Log

As part of the agreement between the US and Russia on manned space flight operations, the first Russian cosmonauts (Mir veterans Sergei Krikalev and Vladimir Titov) arrived at NASA JSC in Houston in late October 1992, to train for STS-60 and STS-63. Their training would be an abbreviated form of NASA mission specialist (not candidate) training, which would include RMS operations and EVA training using American EMU hardware. The training flow for the cosmonauts took into account their vast experience in the Russian programme. In February 1993, Krikalev was assigned the prime position on STS-60 with Titov as his back-up, reversing the roles for STS-63. These flights were the precursor missions that would include up to ten (later reduced to seven) long-duration American residencies on Mir, Shuttle dockings and further Russian cosmonauts incorporated into crews for Shuttle-Mir

STS-60

Russia’s first cosmonaut to fly on the American Shuttle, Sergei Krikalev is seen on the aft flight deck of Discovery during the STS-60 mission. He uses the SAREX equipment to talk with American students in Maine and holds a camcorder for recording in-flight activities

missions. This all fell under Phase 1 of the International Space Station programme, the sixteen-nation cooperative programme that essentially replaced both the US Space Station Freedom and Russian Mir 2 programmes.

The mission of STS-60 had been postponed from November 1993 and resched­uled for January 1994, but a leaking aft RCS thruster in the orbiter forced a further delay while it was investigated. On the third attempt, the launch occurred without incident and the SpaceHab experiments were activated shortly after reaching orbit. The twelve experiments in the programme included four in materials sciences, seven in life sciences and a space dust collection experiment. On the third flight day, the crew attempted to deploy the Wake Shield Facility, but radio interference and problems in reading status information from the facility meant that the attempt had to be abandoned. The following day, the deployment was again cancelled when the facility’s attitude control system developed problems. For two days, the facility remained on the end of the robot arm, conducting abbreviated experiments and being berthed during FD 6. The Wake Shield Facility was planned as a deployable and retrievable experiment platform that would leave a vacuum wake in low-Earth orbit, which was calculated as being 10,000 times greater than that created on Earth in the laboratory. Within this “ultra-vacuum” environment, it was planned to grow defect-free thin film layers of semi-conductor materials (such as gallium arsenide).

Two experiments deployable from GAS canisters (six orbital debris calibration spheres – ranging from 5 to 15 cm in diameter, and a German satellite that measured acceleration forces) were carried on the flight, as well as three other GAS canister experiments. There was also a capillary pump experiment and an auroral photography experiment included in the science package. Krikalev had been given crew roles in photography and TV tasks, as well as maintenance activities during the flight. He supported SpaceHab systems and RMS operations and participated in the Earth observation programme. He was also assigned roles in some of the secondary experi­ments on the mission. His primary role was participation in the joint in-flight medical and radiological investigations. Krikalev also used the SAREX ham radio equipment to talk with operators in Moscow. After a one-orbit waive-off due to unfavourable weather at KSC, the mission ended with a perfect landing, a successful opening of the series of cooperative missions that would lead to the ISS programme.

The most significant achievement was that a cosmonaut could be trained to work with an American crew on an American mission in such a short time. This was a strong reflection of the capabilities of Krikalev, who took to both the English language and the American training system more easily than Titov. It was also a compliment to the vast experience both men brought from their own programme. Krikalev had more than 400 days experience from two missions and Titov had logged a year in space on one mission. The Russians seemed to integrate well with the American programme, but the question now was whether the Americans could do the same when they had to spend far longer in Russia training for a residency on Mir.

Milestones

167th manned space flight 90th US manned space flight 60th Shuttle mission 18th flight of Discovery 1st Russian cosmonaut on Shuttle

1st cosmonaut not to be launched from Baikonur or land in Russian territory 1st flight of Wake Shield Facility 100th Get Away Special (GAS) payload