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SLS A-410
Part of SLS
SLS A-410
SLS A-410
Credit: © Mark Wade
American orbital launch vehicle. The smallest identified member of the SLS family, selected to place the Air Force Lunex lunar lander re-entry vehicle in a low earth orbit for initial tests, was the A-410. This consisted of the 'A' LOx/LH2 stage supplemented by 100-inch diameter solid fuel booster rockets.

AKA: Space Launching System A-410. Status: Study 1961. Payload: 9,070 kg (19,990 lb). Thrust: 7,553.00 kN (1,697,981 lbf). Gross mass: 420,000 kg (920,000 lb). Height: 27.00 m (88.00 ft). Diameter: 7.62 m (24.99 ft). Span: 18.60 m (61.00 ft). Apogee: 560 km (340 mi).

LEO Payload: 9,070 kg (19,990 lb) to a 560 km orbit at 28.00 degrees.

Stage Data - SLS A-410



Family: orbital launch vehicle. Country: USA. Stages: SLS Stage A, SLS SRB 388. Agency: USAF.
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Lunex B-825 LVLunex B-825 LV
Provisional drawing of Lunex B-825 launch vehicle.



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