• Thumbnail for RD-107
    The RD-107 and its sibling, the RD-108, are a type of rocket engine used on the R-7 rocket family. RD-107 engines are used in each booster and the RD-108...
    19 KB (1,176 words) - 22:36, 20 September 2024
  • Thumbnail for NPO Energomash
    Notable examples are the RD-107/RD-108 engines used on the R-7, Molniya and Soyuz rocket families, and the RD-170, RD-171 and RD-180 engines used on the...
    16 KB (1,154 words) - 07:59, 16 December 2023
  • Thumbnail for RD-180
    The RD-180 (Russian: Ракетный Двигатель-180 (РД-180), romanized: Raketnyy Dvigatel-180, lit. 'Rocket Engine-180') is a rocket engine that was designed...
    30 KB (3,224 words) - 22:37, 20 September 2024
  • Thumbnail for Sputnik (rocket)
    Sputnik Rocket Archived 2005-01-03 at the Wayback Machine "РД-107 и РД-108 | RD-107 and RD-108". lpre.de. Retrieved 2015-12-24. "Jonathan McDowell's launch...
    7 KB (651 words) - 22:15, 27 September 2024
  • Thumbnail for Gas-generator cycle
    engineering complexity compared to the staged combustion (closed) cycle. RD-107, RD-108—Soviet engine type developed in the 1950s, used on R-7 family vehicles...
    5 KB (485 words) - 03:51, 10 July 2024
  • Thumbnail for R-7 Semyorka
    powered by the RD-107 engine providing a sea level thrust of 83 tons, each with two vernier engines to assist with steering. The central core's RD-108 engine...
    18 KB (1,844 words) - 12:23, 7 September 2024
  • Thumbnail for Soyuz (rocket)
    basically a Molniya 8K78M sans the Blok L stage and featured the 8D74M RD-107 and the RD-110 engines from the 8K78M, The new, uprated core stage and strap-ons...
    7 KB (588 words) - 19:51, 16 September 2024
  • Thumbnail for NK-33
    the RD-180 of the Atlas V and the four combustion chambers used in the RD-170 of the Energia and Zenit rocket families, and the RD-107, RD-108, RD-117...
    23 KB (2,428 words) - 22:34, 20 September 2024
  • Thumbnail for Soviet rocketry
    engines were powered by the RD-107 engine, each with two Vernier engines to assist with steering. The central core's RD-108 engine included four Vernier...
    55 KB (7,492 words) - 10:50, 22 August 2024
  • Thumbnail for Vostok (rocket family)
    68 m Span: 8.35 m Length: 19.00 m Propellants: Lox/Kerosene Engines: 1 x RD-107-8D74-1959 per booster = 4 Second Stage — Block A (core stage) Gross mass:...
    6 KB (458 words) - 18:41, 24 September 2024
  • Thumbnail for Korabl-Sputnik 2
    oscillations in the RD-107 engine. This had been a problem on earlier R-7 launches but was corrected in the latest revision of the RD-107. The booster used...
    6 KB (636 words) - 03:31, 3 September 2024
  • in the development of the RD-107 and RD-108 liquid-propellant rocket engines for the R-7 rocket family, as well as the RD-270 for the UR-700 launch vehicle...
    3 KB (288 words) - 00:01, 21 March 2024
  • Thumbnail for Klimov RD-33
    The Klimov RD-33 is a turbofan jet engine for a lightweight fighter jet and which is the primary engine for the Mikoyan MiG-29 and CAC/PAC JF-17 Thunder...
    14 KB (1,437 words) - 19:42, 22 August 2024
  • Thumbnail for Dobrynin RD-7
    The Dobrynin RD-7 or "VD-7" is a Soviet single-shaft axial-flow turbojet engine, which was produced in a small series. "RD" means реактивный двигатель...
    3 KB (165 words) - 18:47, 5 March 2023
  • Thumbnail for Vernier thruster
    used verniers. Examples include the RD-8 on the Zenit rocket family, the RD-855 and RD-856 on the R-36, and the RD-0214 on the Proton rocket family. On...
    6 KB (694 words) - 07:38, 10 February 2024
  • Thumbnail for Hydrogen peroxide
    Jupiter, Redstone and Viking used hydrogen peroxide as a monopropellant. The RD-107 engines (used from 1957 to present) in the R-7 series of rockets decompose...
    92 KB (9,247 words) - 05:39, 26 September 2024
  • Thumbnail for Molniya (rocket)
    305,000 kg Strap-On Boosters: Blok-B,V,G,D / 4 × RD-107 Stage 1: Blok-A / RD-108K Stage 2: Blok-I / RD-0108 Stage 3: Blok-L / S1.5400 Molniya rockets were...
    9 KB (443 words) - 18:08, 19 September 2024
  • Thumbnail for De Laval nozzle
    Longitudinal section of RD-107 rocket engine (Tsiolkovsky State Museum of the History of Cosmonautics)...
    15 KB (1,622 words) - 15:46, 27 September 2024
  • Thumbnail for RD-214
    ballistic missile development race, the basic design of the RD-211 also served as basis for the RD-107/RD-108 engine, which went to be the most flown rocket engines...
    11 KB (667 words) - 06:53, 28 April 2024
  • Thumbnail for Soyuz (rocket family)
    (64 feet 4 inches) Burn time: 118 seconds Engines: Soyuz and Soyuz-U models RD-107 Thrust 813 kN (183 klbf) at liftoff Thrust 991 kN (223 klbf) in vacuum Specific...
    27 KB (2,964 words) - 21:01, 12 July 2024
  • Thumbnail for Valentin Glushko
    Shyster). The R-7 ("Semyorka") would include four of Glushko's RD-107 engines and one RD-108. In 1954, he began to design engines for the R-12 Dvina (SS-4...
    17 KB (2,125 words) - 15:18, 18 March 2024
  • the Voskhod program had a man-rated version of the RD-0107 engine; this version was known as the RD-0108. Starting in 1966, the 11A57 adopted the standardized...
    4 KB (297 words) - 21:06, 17 September 2024
  • them and the Blok E stage also had the improved RD-0109 engine to correct some deficiences in the RD-0105 used on earlier 8K78s. It was a member of the...
    5 KB (327 words) - 16:48, 17 September 2024
  • Missiles Unguided rockets Engines RD-8 RD-9 R-11 R-13 R-15 R-25 R-29 RD-33 RD-45 RD-58 RD-107 RD-117 RD-0120 RD-0124 RD-0146 RD-170 RD-180 RD-191 RD-500...
    32 KB (4,044 words) - 22:03, 22 July 2024
  • Thumbnail for Luna (rocket)
    Powered by 1 RD-107-8D74-1958 Maximum thrust 990.00 kN Burn time 120 seconds Propellant Kerosene/LOX Second stage – Block A Powered by 1 RD-108-8D75-1958...
    7 KB (661 words) - 17:44, 24 September 2024
  • Anatoly. "The Soyuz-1 rocket". Russian Space Web. Retrieved 7 March 2010. "RD-107, RD-108". JSC Kuznetsov. Archived from the original on 2015-07-21. Retrieved...
    22 KB (2,526 words) - 04:51, 26 September 2024
  • Thumbnail for Luna E-1 No.1
    1/5, was traced to high frequency combustion instability in the strap-on RD-107 engines, something that would become a persistent problem on R-7 launches...
    5 KB (594 words) - 02:02, 18 September 2024
  • Thumbnail for Rocket engine
    proved a problem on some rocket engines, including the RD-107 engine used in the R-7 family and the RD-216 used in the R-14 family, and several failures of...
    100 KB (11,709 words) - 15:11, 29 September 2024
  • Thumbnail for RD-0110
    The RD-0110 (or RO-8 , RD-0108 , RD-461 ) is a rocket engine burning liquid oxygen and kerosene in a gas generator combustion cycle. It has four fixed...
    12 KB (1,157 words) - 09:34, 19 May 2024
  • Klimov VK-10M 22 to 24,200 lbf (97.87 - 107.647 kN) RD-35 , agreement with Slovakian PSLM ZVL RD-45 GTD-350 RD-500 , copy of the Rolls-Royce Derwent V...
    9 KB (819 words) - 16:59, 22 June 2024