| Hyper III | |
|---|---|
| Role | Lifting-body remotely piloted vehicle |
| National origin | United States |
| Manufacturer | National Aeronautics and Space Administration |
| Designer | Dale Reed |
| First flight | 12 December 1969 |
| Primary user | NASA |
| Number built | 1 |
The NASA Hyper III was an American unpowered full-scale lifting body remotely piloted vehicle designed and built at the NASA Flight Research Center at Edwards Air Force Base, California.[1]
The Hyper III was designed to help in the M2 lifting body program, it had a flat bottom and sides and a simple straight wing with no flaps, ailerons or any control surfaces.[1] The wing was designed to simulate a pop-out wing that had been proposed for a re-entry vehicle. It had twin fins and rudders canted at 40° from the vertical with hinged elevons on the horizontal surface.[1] The landing gear was a fixed tricyle type, using spring steel legs from a Cessna aircraft.[1] It was fitted with an emergency parachute system and the aircraft was controlled by 5-channel radio link, instrument data was down-linked using a 12-channel radio.[1]
On the 12 December 1969 the Hyper III was launched from a helicopter at 10,000 feet. It glided 5 km, turned round, came back and landed. After the three-minute flight it was not flown again as the Center cancelled the program.[1]
Data from Jane's All the World's Aircraft 1973-74[1]
General characteristics
Performance
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