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
NLS HLV
Part of NLS
NLS - Martin NLS - Martin Marrietta 'stage-and-a-half' design Credit: Lockheed Martin |
American heavy-lift orbital launch vehicle. NLS Heavy Lift Version. Lower cost expendable launch vehicle studied by NASA/USAF in late 1980's.
AKA: National Launch System;New Launch System. Status: Study 1991. Thrust: 11,791.00 kN (2,650,722 lbf). Gross mass: 833,732 kg (1,838,064 lb). Height: 62.00 m (203.00 ft). Diameter: 8.70 m (28.50 ft).
Flyaway Unit Cost 1985$: 59.000 million.
Stage Data - NLS HLV
- Stage 1. 1 x NLS HLV. Gross Mass: 833,732 kg (1,838,064 lb). Empty Mass: 62,757 kg (138,355 lb). Thrust (vac): 14,310.000 kN (3,217,010 lbf). Isp: 425 sec. Burn time: 221 sec. Isp(sl): 350 sec. Diameter: 8.70 m (28.50 ft). Span: 8.70 m (28.50 ft). Length: 52.00 m (170.00 ft). Propellants: Lox/LH2. No Engines: 4. Engine: STME. Other designations: National Launch System. Status: Study 1991.
Family:
heavy-lift,
orbital launch vehicle.
Country:
USA.
Engines:
STME.
Stages:
NLS HLV stage.
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