Encyclopedia Astronautica 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 OOST ISI stage AKA: OOST ISI. Status: Study 1963. Thrust: 85,386.00 kN (19,195,536 lbf). Gross mass: 5,125,000 kg (11,298,000 lb). Unfuelled mass: 292,000 kg (643,000 lb). Specific impulse: 455 s. Specific impulse sea level: 365 s. Burn time: 248 s. Height: 57.90 m (189.90 ft). Diameter: 21.30 m (69.80 ft). Span: 21.30 m (69.80 ft).
Cost $ : 117.600 million. No Engines: 15.
Country: USA. Engines: Chamber/single nozzle. Launch Vehicles: OOST ISI. Propellants: Lox/LH2. 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 � 1997-2016 Mark Wade - Contact � / Conditions for Use |
