Lavochkin La-7PVRD and La-9RD

Lavochkin La-7PVRD and La-9RD

Purpose: To investigate the use of pulsejets to boost fighter performance.

Design Bureau: The OKB of Semyon A Lavochkin.

In 1942 Vladimir N Chelomey, working at TsIAM (Central Institute of Aviation Motors) began bench-testing the first pulsejet in the Soviet Union. This was independent of work by the German Argus company, which be­cause of Soviet secrecy became famed as the pioneer of such engines. The Soviet unit re­ceived two designations, D-10 and RD-13. In 1946 the first two flight-cleared D-10 engines were hung under the wings of a slightly mod­ified La-7, which was designated La-7PVRD. In the second half of 1947 a second pair, des­ignated RD-13, were flown under the wings of an La-9, which misleadingly received the des­ignation La-9RD. Despite the fact that the pro­gramme had already been abandoned, eight further La-9 fighters were fitted with these en­gines, and all nine made a deafening forma­tion flypast at the Tushino Aviation Day.

Left: La-7/2D-10.

The D-10 pulsejet appears to have been heavier than the German 109-014 unit of sim­ilar size, though weight data are lacking. The duct was mainly aluminium at the front and steel to the rear ofthe fuel injectors. Fuel was drawn from the main aircraft tanks and igni­tion was electrical. The unit was suspended from a shallow pylon projecting ahead of the wing leading edge with two main attach­ments, with a steadying attachment at the rear. Apart from the pulsejet instrumentation and control system a few modifications were needed to the aircraft, the main one being to remove a large portion of flap above the pulsejet jetpipe. No data are available de­scribing how thrust varied with airspeed or height; Shavrov merely gives the thrust of a single D-10 as 200kg (44 lib).

Подпись: La-9RD, also called La-9D-13 orLa-9/2D-13Lavochkin La-7PVRD and La-9RDLavochkin La-7PVRD and La-9RDThough these pulsejets performed as ex­pected, they significantly added to aircraft weight and drag, and reduced manoeuvrabil­ity, especially rate of roll. In addition, the vio­lent vibration transmitted to the aircraft ‘made flying difficult’ and was very unpopular with pilots.

Dimensions (La-7PVRD)

Span

9.8m

32 ft % in

Length

8.6m

28 ft n in

Wing area

17.59m2

189ft2

Weights

Empty

2,998kg

6,609 Ib

Loaded

3,701 kg

8,159 Ib

Performance

Maximum speed, according to Shavrov the calculated speeds were

800 km/h at 6,000 m and 715 km/h at 8,000

m, whereas the actual

speeds at these heights were

670 km/h (416 mph) and 620 km/h

(385 mph), or marginally lower than without the pulsejets!

 

Dimensions (La-9RD)

Span

Length

Wing area

9.8m

8.63m

17.72m2

32ftP/Un 28 ft 3% in 191 ft2

Weights

Empty

3,150kg

6,944 Ib

Loaded

3,815kg

8,410 Ib

Performance

Maximum speed, the calculated gain was 127 km/h, but Shavrov gives the actual achieved speed as 674 km/h (419 mph), 16 km/h slower than the original La-9.

 

Right: Three views of La-9RD.

 

Lavochkin La-7PVRD and La-9RD