Helios Stage 1

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

Helios Stage 1

Notional LOx/LH2 rocket engine. Study 1960. Engines for booster stage with LOx tanks only to take nuclear second stage to stratosphere. Helios A, B, C studies.

Status: Study 1960. Thrust: 1,667.00 kN (374,756 lbf). Specific impulse: 400 s. Specific impulse sea level: 340 s. Burn time: 117 s.

Country: USA. Launch Vehicles: Helios A, Helios B, Helios C. Propellants: Lox/LH2. Stages: Helios A-1, Helios B-1, Helios C-1.

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