Northrop HL-10
| Use attributes for filter ! | |
| Top speed | 1,976 km/h |
|---|---|
| Retired | July 17, 1970 |
| Range | 72 km |
| Wingspan | 4. 15 m |
| Engine types | Reaction Motors XLR11 |
| First flight | December 22, 1966 |
| Date of Reg. | |
| Date of Upd. | |
| ID | 1721162 |
About Northrop HL-10
The Northrop HL-10 was one of five US heavyweight lifting body designs flown at NASA's Flight Research Center in Edwards, California, from July 1966 to November 1975 to study and validate the concept of safely maneuvering and landing a low lift-over-drag vehicle designed for reentry from space.
