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...

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...

The RD-180 (Russian: Ракетный Двигатель-180 (РД-180), romanized: Raketnyy Dvigatel-180, lit. 'Rocket Engine-180') is a rocket engine that was designed...

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...

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...

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...

the original Blok I stage as developed in 1960 used RD-107 engines, the Soyuz boosters instead had RD-110s, which were more powerful as necessitated by...

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...

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:...

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...

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...

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...

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...

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...

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...

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...

Longitudinal section of RD-107 rocket engine (Tsiolkovsky State Museum of the History of Cosmonautics)...

(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...

over the RD-107; however, only a limited number of engines are available. Once the supply is exhausted, the NK-33 will be replaced by the RD-193. In April...

Blok I stage in the Voskhod booster used the RD-0107 engine rather than the crew-rated and more powerful RD-0110 used on the Soyuz. The sole exceptions...

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...

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...

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...

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...

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...

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...

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...

Powered by 1 RD-107-8D74-1959 Maximum thrust 970.86 kN Total thrust 3883.4 kN Burn time 118 seconds Propellant RP-1/LOX First stage Powered by 1 RD-108-8D75-1959...

pp. 779–781. Retrieved 22 July 2022. ЖРД РД-107 и РД-108 и их модификации [Liquid Rocket Engines RD-107/108 and their modifications]. www.lpre.de (in...

had been copied without license to power the MiG-15 'Fagot', first as the RD-45, and after initial problems of metallurgy forced the Soviet engineers to...