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-0201
Part of RD-0200 Family
Kosberg Nitric acid/Amine rocket engine. SAM V1100 by Grushin stage 3. Out of Production. Thrust range 59 - 28 kN. First flight 1960.

Status: Out of Production. Date: 1957-60. Thrust: 58.06 kN (13,052 lbf). Unfuelled mass: 120 kg (260 lb). Specific impulse: 260 s. Burn time: 180 s. Height: 0.70 m (2.29 ft). Diameter: 0.40 m (1.31 ft).

Chambers: 4. Throttled thrust(vac): 28.000 kN (6,294 lbf). Engine: 120 kg (260 lb). Chamber Pressure: 62.00 bar. Propellant Formulation: AK27P/TG-02. Thrust to Weight Ratio: 49.33.



Family: Storable liquid. Country: Russia. Propellants: Nitric acid/Amine. Agency: Kosberg bureau. Bibliography: 307, 342.

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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use