SRM-2 (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

SRM-2

IUS

IUS
Credit: NASA

CSD solid rocket engine. Used in Shuttle, Titan 34D; IUS-2. Known by manufacturer as Orbus 6. First flight 1982.

AKA: IUS-2;Orbus 6. Status: Retired 2004. Number: 58 . Thrust: 78.40 kN (17,625 lbf). Gross mass: 3,919 kg (8,639 lb). Unfuelled mass: 1,170 kg (2,570 lb). Specific impulse: 304 s. Specific impulse sea level: 200 s. Burn time: 103 s. Height: 2.08 m (6.82 ft). Diameter: 1.61 m (5.28 ft).

Thrust (sl): 51.600 kN (11,600 lbf). Thrust (sl): 5,261 kgf.

Country: USA. Launch Vehicles: Titan 34D/IUS, Titan 34D, Titan 402A/IUS, Commercial Titan 3, Titan 405A, Titan 402B/IUS. Propellants: Solid. Stages: SRM-2. Agency: CSD.

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