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Saturn II-INT-17


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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 Saturn II-INT-17 Part of Saturn II LOx/LH2 propellant rocket stage. Saturn II modified with reduced expansion ratio HG-3 high pressure engines for use a first stage (sea level launch).

Status: Study 1966. Thrust: 9,713.40 kN (2,183,659 lbf). Gross mass: 495,000 kg (1,091,000 lb). Unfuelled mass: 48,000 kg (105,000 lb). Specific impulse: 450 s. Specific impulse sea level: 275 s. Burn time: 200 s. Height: 24.84 m (81.49 ft). Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft).

No Engines: 7.

Country: USA. Engines: HG-3-SL. Launch Vehicles: Saturn INT-17. Propellants: Lox/LH2. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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