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 MM T10RR-2
Part of Nova
Nova Model T10RR-2
Nova Model T10RR-2
Nova Martin Marietta Model T10RR-2
Credit: © Mark Wade
American heavy-lift orbital launch vehicle. Two stage Nova using CD modules; reusable first stage with 24 modules exhausting to a zero length plug nozzle; reusable second stage with a toroidal plug nozzle engine. Operational date would have been December 1976.

Status: Study 1963. Payload: 479,000 kg (1,056,000 lb). Thrust: 157,506.70 kN (35,408,915 lbf). Gross mass: 11,704,800 kg (25,804,600 lb). Height: 81.00 m (265.00 ft). Diameter: 21.30 m (69.80 ft). Apogee: 185 km (114 mi).

LEO Payload: 479,000 kg (1,056,000 lb) to a 185 km orbit.

Stage Data - Nova MM T10RR-2



Family: heavy-lift, orbital launch vehicle. Country: USA. Engines: CD Module, Toroid FD. Stages: Nova MM T10RR-2-1, Nova MM T10RR-2-2. Agency: Martin.

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