RD-0216 (original) (raw)

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z

RD-0216

RD-0216
Credit: KBKhA

Kosberg N2O4/UDMH rocket engine. UR-100 stage 1. Staged combustion cycle. Includes tank pressurization system (RD-0217 without tank press.). First launch November 1963, manufactured until 1974, operational until 1991. First flight 1965.

AKA: 15D2. Status: Design 1964. Date: 1963-66. Number: 1128 . Thrust: 219.00 kN (49,233 lbf). Specific impulse: 313 s.

Chamber Pressure: 147.00 bar.

Subtopics

RD-0217 Kosberg N2O4/UDMH rocket engine. UR-100, UR-100K stage 1. Out of Production. Staged combustion cycle. Version of RD-0216 without tank pressurization system. Manufacturing until 1974, operational use until 1991.

	RD-0235 Kosberg N2O4/UDMH rocket engine. UR-100N / RS-18 (SS-19) stage 2. Main engine based on RD-0217 with larger nozzle for altitude operation. Staged combustion cycle. First flight 1972.

Family: Storable liquid. Country: Russia. Launch Vehicles: Taran, UR-100M SLBM, UR-100, UR-100M. Propellants: N2O4/UDMH. Stages: 8S816. Agency: Kosberg bureau. Bibliography: 342, 344, 7484.

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z