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NLS HLV
Part of NLS
NLS - Martin
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



Family: heavy-lift, orbital launch vehicle. Country: USA. Engines: STME. Stages: NLS HLV stage.

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