Category Dreams, Technology, and Scientific Discovery

Opening space research : dreams, technology, and scientific discovery

T

his book is a participant’s well-told and perspective account of the early days of scientific research in space, with emphasis on the role of the University of Iowa. The unique core of the book, Chapters 5-11, is the inside story of the development of the radiation instruments that were flown successfully on the first American Satellite Explorer I and its prompt successor, Explorer III, both in early 1958. The author, George H. Ludwig, then a graduate student in physics at the University of Iowa, was the central person in developing those instruments and in overseeing the decoding and tabulation of their in-flight data. His detailed narrative of this work has a special authenticity because of its dependence on his own meticulous records.

During 1955 and 1956, I prepared proposals for a comprehensive global and tempo­ral survey of the primary cosmic radiation above the Earth’s atmosphere. My proposal was accepted by the U. S. National Committee for the 1957-1958 International Geo­physical Year (IGY) on 12 May 1956 and was placed on the short list of potential payloads for early satellite missions. Initial funding was provided by the National Science Foundation and by my ongoing grant from the U. S. Office of Naval Research.

I specified the scheme of the instrumentation and selected the basic detectors, Geiger-Muller tubes, developed by Nicholas Anton of the Anton Electronics Labora­tories of Brooklyn, New York. The tubes were based on the earlier work of Herbert Friedman in introducing a small admixture of chlorine gas into an argon-filled tube, a so-called halogen quenched tube of “infinite” lifetime and stable operation over a wide range of temperature. Our adopted Anton type 314 tube had these properties and was of mechanically rugged construction.

During 1956-1957, Ludwig mastered the then new techniques of transistor elec­tronics and carried out the detailed design of the electronics for our instruments. He also designed a miniature, commandable magnetic-tape recorder for recording

ix

OPENING SPACE RESEARCH

and rapidly playing back the data from a full satellite orbit in order to obtain com­prehensive geographical and temporal coverage of the counting rate of the Geiger tube.

At the outset of the IGY, the planned vehicle for launching satellites was a Van­guard, under development by the Naval Research Laboratory and the Glenn L. Martin Company. I followed its development closely and also maintained contact with Ernst Stuhlinger of the Army Ballistic Missile Agency (ABMA) on a technically com­petitive but unofficial plan for a multistage ABMA/Jet Propulsion Laboratory (JPL) vehicle. Because of my progressive uneasiness about the difficulties in developing the Vanguard vehicle, Ludwig and I decided that the Iowa instruments would be de­signed for compatibility with either the Vanguard or the ABMA vehicle, later called Jupiter C.

All of our preparatory work culminated in the late autumn of 1957 following success of the Soviet Sputniks 1 and 2, early failures of the Vanguard vehicle, and the consequent national decision to adopt the Jupiter C as a backup vehicle. JPL was assigned overall responsibility for the payload, and the U. S. IGY staff chose the Iowa package as the primary scientific instrument thereof.

In mid-November 1957, Ludwig drove his family from Iowa City to Pasadena, California, with his precious instrumentation in the trunk of their personal automobile in order to work with the JPL staff in integrating it into the payload of the Jupiter C.

The successful launch of Explorer I on 31 January 1958 and Explorer III on 26 March 1958 placed our radiation instruments in space. After several weeks of intense puzzlement in understanding our data, my colleagues and I recognized that we had discovered the presence of an enormous population of energetic, electrically charged particles trapped in the external magnetic field of the Earth—later called the radiation belts. The in-flight reliability of Ludwig’s instruments was central to this discovery.

Ludwig continued at the University of Iowa with the development of radiation instruments for subsequent satellite flights and later had a distinguished career as a senior official of the National Aeronautics and Space Administration and the National Oceanic and Atmospheric Administration.

James A. Van Allen University of Iowa October 2004

OPENING SPACE RESEARCH

FIGURE 0.1 The diminutive Explorer I sitting atop its Jupiter-C launch vehicle just moments before lift-off. The first stage liquid oxygen tank is frosted and still venting, and the upper-stage cylindrical tub and pencil-like satellite are spinning. (Courtesy of the NASA Marshall Space Flight Center.)

Prologue

Cape Canaveral, Florida, 10:47 EST, 31 January 19581

The launch countdown was in its final few minutes, and the cylindrical “tub” atop the first stage of a Juno I launch vehicle was spinning rapidly. Finally, a voice over the intercom intoned, “four – three – two – one – ignition – liftoff.” My senses were soon overwhelmed by the thunder of the rocket engine, as it beat upon me to affirm ignition and the beginning of the rocket’s purposeful climb toward space.

At the very tip of that multistage rocket assembly was a payload containing a cosmic ray instrument that I had painstakingly designed over the past two years as a graduate

xi

xii OPENING SPACE RESEARCH

student at the University of Iowa.2 Perched on a stool in a nearby hangar, I listened with growing satisfaction to a wavering tone from a receiver on the workbench before me. During the 10 minutes following liftoff, the signal told me that the counting rate of the instrument’s Geiger-Muller detector increased, peaked, and then dropped slightly to an essentially constant value.

That counter was detecting showers of secondary atomic particles produced by collisions of high-energy galactic cosmic rays with molecules in the Earth’s upper atmosphere. Its counting rate increased as the instrument rose to a height of about 60,000 feet (11 miles or 18 kilometers),3 where the production of secondary particles peaked. As the counter progressed higher above the substantial atmosphere, it detected fewer and fewer of those secondary particles until, ultimately, the counter registered little other than externally arriving primary cosmic rays.4 5

Thus, the signal’s pattern told me that the rocket had successfully climbed to a height of at least 11 miles, passed above it, and remained above that height until it passed out of range. Furthermore, it showed that the instrument and transmitters in the payload were operating properly.

Down-range tracking stations quickly confirmed that the four-stage rocket had completed its work in lifting the 18 pound payload with my precious instrument package to the intended height of about 220 miles and in propelling it to the required speed of slightly more than 18,000 miles per hour. Although those down-range stations were able to measure the approximate speed of the departing final rocket stage and instrument, they were not capable of accurately determining its exact direction of flight. Thus, it remained possible that it had been aimed excessively upward or downward, in which case it would make a premature fiery descent into the atmosphere. Although preliminary indications of a successful launch looked promising, we still did not know whether the instrument was in a durable orbit.

By that time, there was nothing more that I could learn in the hangar, and I quickly made my way to the project’s more complete receiving station. Located in a special trailer some distance from the other Cape facilities, this was one of a global network of stations setup to receive the signals from the U. S. satellites. That station was especially important at that moment because it was linked to the rest of the receiving station network by high-quality telephone lines. That communication network permitted us to hear of the progress in acquiring the signal as the instrument progressed above other stations around the world. I joined a steadily growing and increasingly excited group at the trailer’s steps.

We did not expect to hear a meaningful confirmation that the instrument had been successfully orbited until it had made a nearly complete circle of the Earth, when it would come within range of receiving stations on the west coast of the North American continent. Expectations were that it would pass within range of four stations in California between 12:25 and 12:30 EST.

PROLOGUE xiii

The time of anticipated signal acquisition came with great excitement but passed with the disappointing absence of any signal. During the next minutes, we waited with a growing dread that the launch or instrument might have failed. Just as my fear was peaking, at about 12:42 EST, a voice from the trailer shouted, “Gold [the Earthquake Valley receiving station] has it!” We knew then that the rocket had provided a greater thrust than expected, resulting in a higher orbit. Thus, it took longer than expected for the new satellite to orbit the Earth. Our knot of observers exploded with applause and shouts of relief and jubilation as we realized that

Подпись: Explorer I, the United State’s first artificial satellite of the Earth, was in orbit!

Joy also reigned in Washington, D. C. The three primary leaders of the effort, Wernher von Braun, directing the booster rocket effort, William H. Pickering, leading the upper-stage rocket and overall satellite effort, and James A. Van Allen, the principal scientist for our cosmic ray experiment, along with a bevy of Army generals, followed the launch and the interminable wait in a “war room” in the Pentagon. As soon as the orbit had been confirmed, the three were whisked to the National Academy of Sciences building on Constitution Avenue. There they briefed several civilian program officials and then led a spirited press conference in the academy’s Great Hall.

Word of the accomplishment immediately spread worldwide, as the front pages of the morning papers were emblazoned with the welcome news.

That event signaled both a conclusion and a beginning. On the national scale, it represented the culmination of a major effort to orbit the first U. S. artificial earth satellite. In Iowa City, it marked the realization of James A. Van Allen’s long-standing dream of placing cosmic ray instruments well above the Earth’s atmosphere. On a personal note, it was the end of a busy and exciting two year developmental effort that later served as the basis for my physics master’s thesis.

The event initiated a new era of scientific research within the Earth’s magnetic shell and beyond. The ensuing half-century of remarkably active and productive research in space has included the conduct of countless scientific investigations throughout our solar system, the announcement of numerous important scientific discoveries, and the training of many scientists who became leaders in the new field.

How did we get to this point, and what followed the initial excursion into space?

Endnotes

1 The corresponding universal time (UT, also commonly referred to as Greenwich Mean Time (GMT)) was 03:47 on 1 February 1958. Local times are used throughout most of this

xiv OPENING SPACE RESEARCH

book. However, in discussions of the worldwide network of ground receiving stations and the data produced by them, the author reverts to universal time to avoid confusion. Such occurrences are appropriately identified.

2 During the period covered in this work, the university was known as the State University of Iowa (SUI), sometimes rather derisively pronounced “soo-eee.” Several decades ago it came to be known, simply, as the University of Iowa (UI). The two names are used here synonymously, with SUI being preferred when describing the events of the 1950s.

3 U. S. units of measure are used throughout most of this book, occasionally with correspond­ing international (SI) units indicated in parentheses.

4 An excellent summary of the state of knowledge of cosmic ray physics at that time is contained in D. J. X. Montgomery, Cosmic Ray Physics (Princeton Univ. Press, 1949).

5 The manner in which the counting rate of a simple Geiger-Muller counter varies as a function of altitude is described in many sources, including James A. Van Allen, “The Cosmic Ray Intensity Above the Atmosphere Near the Geomagnetic Pole,” II Nuovo Cimento (1953) pp. 630-647.