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
Nova-1 DAC
Part of Bono
Nova Douglas 1
Nova Douglas 1
Nova Douglas Aircraft Model 1
Credit: © Mark Wade
American heavy-lift orbital launch vehicle. Douglas/Bono design for Nova using LOx/RP-1 in first stage, existing engines.

Status: Study 1963. Payload: 454,500 kg (1,002,000 lb). Thrust: 85,079.10 kN (19,126,543 lbf). Gross mass: 7,026,400 kg (15,490,500 lb). Height: 64.00 m (209.00 ft). Diameter: 21.30 m (69.80 ft). Apogee: 325 km (201 mi).

LEO Payload: 454,500 kg (1,002,000 lb) to a 325 km orbit.

Stage Data - Nova-1 DAC



Family: heavy-lift, orbital launch vehicle. Country: USA. Engines: 5 mlbf RP-4, M-1. Stages: Nova DAC-1, Nova DAC-2. Agency: Douglas.
Photo Gallery

Nova  -  DouglasNova - Douglas
Nova Concepts - Douglas Aircraft
Credit: © Mark Wade



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