Operator | NASA |
---|---|
Applications | Crewed spaceplane |
Specifications | |
Launch mass | 10,884 kg (23,995 lb) |
Regime | Low Earth |
Production | |
Status | Cancelled |
Launched | 0 |
Related spacecraft | |
Derivatives | HL-42, Dream Chaser |
The HL-20 Personnel Launch System was a NASA spaceplane concept for crewed orbital missions studied by NASA's Langley Research Center around 1990. It was envisaged as a lifting body re-entry vehicle similar to the Soviet BOR-4 spaceplane design.[1] Its stated goals were to achieve low operational costs, improved flight safety, and a possibility of landing on conventional runways.[2] No flight hardware was built.