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 DAC ISI
Part of Bono
American heavy-lift orbital launch vehicle. Douglas/Bono design for Nova using LH2/LOx in both stages. Improved Specific Impulse chemical stage uses many engines feeding into single large nozzle.

Status: Study 1963. Payload: 454,500 kg (1,002,000 lb). Thrust: 64,134.40 kN (14,417,987 lbf). Gross mass: 5,325,400 kg (11,740,400 lb). Height: 73.00 m (239.00 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 DAC ISI



Family: heavy-lift, orbital launch vehicle. Country: USA. Engines: Chamber/single nozzle. Stages: Nova DAC ISI-1, Nova DAC ISI-2. Agency: Douglas.

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