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
DAC Helios-1
Part of DAC Helios
LOx/LH2 propellant rocket stage. .

Status: Study 1963. Thrust: 52,926.00 kN (11,898,238 lbf). Gross mass: 1,660,000 kg (3,650,000 lb). Unfuelled mass: 149,000 kg (328,000 lb). Specific impulse: 410 s. Specific impulse sea level: 345 s. Burn time: 113 s. Height: 16.20 m (53.10 ft). Diameter: 24.40 m (80.00 ft). Span: 29.00 m (95.00 ft).

No Engines: 4.



Country: USA. Engines: Chamber/single nozzle. Launch Vehicles: DAC Helios. Propellants: Lox/LH2.

Back to top of page
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
© 1997-2019 Mark Wade - Contact
© / Conditions for Use