Wikipedia

Gas Dynamics Laboratory

Gas Dynamics Laboratory (GDL) (Russian: Газодинамическая лаборатория) was the first Soviet research and development laboratory to focus on rocket technology. Its activities were initially devoted to the development of solid propellant rockets, which became the prototypes of missiles in the Katyusha rocket launcher, as well as liquid propellant rockets, which became the prototypes of Soviet rockets and spacecraft. At the end of 1933 it became part of the Reactive Scientific Research Institute (RNII). A number of craters on the far side of the Moon are named after GDL employees.

Gas Dynamics Laboratory "GDL"
The building of the Main Admiralty in Leningrad, where in the 1930s the Gas Dynamics Laboratory was located
Parent institutionRevolutionary Military Council of the USSR
Founder(s)Nikolai Tikhomirov
Established1921[1]
Missionresearch and development
FocusSolid-propellant rockets, Liquid-propellant rockets
Key peopleValentin Glushko
Location
USSR, Moscow and Leningrad
Dissolvedin 1933 became RNII
Nikolai Tikhomirov, creator of GDL
Valentin Glushko
Georgy Langemak

History of the organization

edit

GDL Managers

edit

Nikolai Tikhomirov (1921—1930);

Boris Sergeevich Petropavlovsky [ru] (1930-1931);

Nikolai Yakovlevich Ilyin (rocket scientist) [ru] (1931—1932);

Ivan Kleymyonov (12.1932 - 9.1933, then head of the RNII).

Solid propellant rockets

edit

The GDL utilised smokeless (TNT) gunpowder on a non-volatile solvent for solid propellant rockets. The first test-firing of a solid fuel rocket was carried out in March 1928, which flew for about 1,300 meters[4] In 1931 the world's first successful use of rockets to assist take-off of aircraft were carried out on a U-1, the Soviet designation for an Avro 504 trainer, which achieved about one hundred successful assisted takeoffs.[5][6] Successful assisted takeoffs were also achieved on the Tupolev TB-1 (Russian 'ТБ-1')[4] and Tupolev TB-3 aircraft.[5][3] Further developments in the early 1930s were led by Georgy Langemak,[1] including firing rockets from aircraft and the ground. In 1932 in-air test firings of RS-82 missiles from a Tupolev I-4 aircraft armed with six launchers successfully took place.[3] RNII then modified these rockets for the famous Katyusha rocket launcher,[7] which were used during World War II. In these works, the main design contribution was made by GDL employees Nikolai Tikhomirov, Vladimir Artemyev, Boris Petropavlovsky, Georgy Langemak, Ivan Isidorovich and others.[2]

Electric & liquid fuel rocket engines

edit

On 15 May 1929 a section was created to develop electric rocket engines, headed by 23 year old Valentin Glushko,[2][8][1] Glushko proposed to use energy in electric explosion of metals to create rocket propulsion.[5] In the early 1930s the world's first example of an electrothermal rocket engine was created.[9][3] This early work by GDL has been steadily carried on and electric rocket engines were used in the 1960s onboard the Voskhod 1 spacecraft and Zond-2 Venus probe.[5]

In 1931 Glushko was redirected to work on liquid propellant rocket engines.[1] This resulted in the creation of ORM (from "Experimental Rocket Motor" in Russian) engines ORM-1 [ru] to ORM-52 [ru].[5] To increase the resource, various technical solutions were used: the jet nozzle had a spirally finned wall and was cooled by fuel components, curtain cooling was used for the combustion chamber[9] and ceramic thermal insulation of the combustion chamber using zirconium dioxide.[2] Nitric acid, solutions of nitric acid with nitrogen tetroxide, tetranitromethane, hypochloric acid and hydrogen peroxide were first proposed as an oxidizing agent.[2] As a result of experiments, by the end of 1933, a high-boiling fuel from kerosene and nitric acid was selected as the most convenient in operation and industrial production.[9] In 1931 self-igniting combustible and chemical ignition of fuel with gimbal engine suspension were proposed.[2] For fuel supply in 1931-1932 fuel pumps operating from combustion chamber gases were developed. In 1933 a centrifugal turbopump unit for a rocket engine with a thrust of 3000 N was developed.[2] A total of 100 bench tests of liquid-propellant rockets were conducted using various types of fuel, both low and high-boiling and thrust up to 300 kg was achieved.[4][5]

Experimental liquid propellant rockets were constructed, the first two rockets with a planned lifting height of 2–4 km were manufactured[9] and testing was continued by RNII.[10]

The work on the creation of engines under the leadership of Glushko was carried out by employees of the ERD and liquid-propellant engine section, including the active involvement of A. L. Maly, V. I. Serov, E. N. Kuzmin, I. I. Kulagin, E. S. Petrov, P. I. Minaev, B. A. Kutkin, V. P. Yukov, N. G. Chernyshev and others.[2][5]

Location of the laboratory in Leningrad in the 1930s

edit

Lunar craters named after GDL employees

edit

In 1966, the Commission of the USSR Academy of Sciences on Lunar Names assigned craters on the far side of the Moon names in honor of the following workers of the GDL; Nikolai Tikhomirov, N. P. Alyokhina, Vladimir Artemyev, Artamonova, A. I. Gavrilova, A. D. Gracheva, Zhiritsky, A. L. Maly, Y. B. Mezentseva, E. S. Petropavlovsky, B.S. Petrova, G. F. Firsova, N. G. Chernysheva. In 1962 the names GDL, GIRD and RNII were assigned to crater chains on the far side of the Moon.[8][9]

Museum of Cosmonautics and Rocket Technology named after V. P. Glushko

edit
 
RLA-1 rocket in the Museum of Cosmonautics and Rocketry (in the Peter and Paul Fortress)

The V. P. Glushko Museum of Cosmonautics and Rocket Technology [ru] is a memorial museum telling about the beginning of the domestic space engine industry, including the history of GDL. The museum is located in the Peter and Paul Fortress, which in the 1930s housed GDL stands for testing rocket engines. It was opened on April 12, 1973.[11][12]

See also

edit

Notes

edit

References

edit
  1. ^ a b c d e f g Siddiqi, Asif (2000). Challenge to Apollo : the Soviet Union and the space race, 1945-1974 (PDF). Washington, D.C: National Aeronautics and Space Administration, NASA History Div. pp. 6–7. Retrieved 22 May 2022.
  2. ^ a b c d e f g h i j k Gas-Dynamic Laboratory, Great Soviet Encyclopedia (1926–1981 (printed version) ed.). Sovetskaya Entsiklopediya. December 1973. ISBN 9780028800004.
  3. ^ a b c d e Chertok, Boris (31 January 2005). Rockets and People (Volume 1 ed.). National Aeronautics and Space Administration. pp. 164–165. Retrieved 29 May 2022.
  4. ^ a b c Zak, Anatoly. "Gas Dynamics Laboratory". Russian Space Web. Retrieved 29 May 2022.
  5. ^ a b c d e f g Glushko, Valentin (1 January 1973). Developments of Rocketry and Space Technology in the USSR. Novosti Press Pub. House. pp. 6–7, 11–12. OCLC 699561269.
  6. ^ У-1 на сайте airwar.ru — «Уголок неба»
  7. ^ "Katyusha rocket launcher. Weapon of Victory: multiple launch rocket system "Katyusha"". ezoteriker. Retrieved 5 June 2022.
  8. ^ a b Brief chronology of rocket engine building in the USSR
  9. ^ a b c d e "Gas Dynamic Laboratory (in Russian)". History of Russian Soviet Cosmonautics. Retrieved 10 June 2022.
  10. ^ Zak, Anatoly. "History of the Rocket Research Institute, RNII". Russian Space Web. Retrieved 10 June 2022.
  11. ^ "Museum of space exploration and rocket technology V. P. Glushko". State Museum of the history of St Petersburg. Retrieved 10 June 2022.
  12. ^ "Museum of Cosmonautics and Rocket Technology Glushko, Peter and Paul Fortress, St. Petersburg". life-globe.com. Retrieved 10 June 2022.

Further reading

edit
  • Glushko V. P. Academy of Sciences of the USSR. Rocket engines GDL - OKB;
  • Petrovich G. V. Development of Rocket Engineering in the USSR. Ch. 1—2. — M., 1968;
  • Petrovich G. V. Rocket engines GDL — OKB, 1929—69. — M., 1969;
  • Cosmonautics: A Small Encyclopedia. — 2nd ed. — M., 1970.
Retrieved from "https://en.wikipedia.org/w/index.php?title=Gas_Dynamics_Laboratory&oldid=1254987783"