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Shuttle C stage


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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 Shuttle C stage Part of Shuttle Orbiter N2O4/MMH propellant rocket stage. .

AKA: IHLLV;Interim Heavy Lift Launch Vehicle;Shuttle C. Status: Study 1989. Thrust: 6,834.30 kN (1,536,412 lbf). Gross mass: 36,360 kg (80,160 lb). Unfuelled mass: 34,380 kg (75,790 lb). Specific impulse: 313 s. Burn time: 120 s. Height: 21.00 m (68.00 ft). Diameter: 6.30 m (20.60 ft). Span: 6.30 m (20.60 ft).

Cost $ : 9.570 million. No Engines: 2.

Country: USA. Engines: OME. Launch Vehicles: IHLLV, Shuttle C. Propellants: N2O4/MMH. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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