“NASA Hyper III”的意思、由来-开放百科全书

词条

NASA Hyper III

释义

Design and development
Specifications
See also
References
Notes Bibliography
External links

name=Hyper III

image=Hyper III at Dryden 1969.jpg

caption=

}}{{Infobox aircraft type

type=Lifting-body remotely piloted vehicle

national origin=United States

manufacturer=National Aeronautics and Space Administration

designer=Dale Reed

first flight=12 December 1969

introduced=

retired=

status=

produced=

primary user=NASA

number built=1

developed from=

variants with their own articles=

developed into=
}}

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.

Design and development

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 control surfaces that was designed to simulate a pop-out wing that had been proposed for a re-entry vehicle. The Hyper III had twin fins and rudders canted at 40° from the vertical, and hinged elevons on the horizontal surface. The landing gear was a fixed tricycle type, using spring steel legs from a Cessna aircraft. It was fitted with an emergency parachute system and controlled by 5-channel radio link; instrument data was downlinked using a 12-channel radio.

On 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.

Specifications

{{aerospecs
|ref=Jane's All the World's Aircraft 1973-74
|met or eng?=eng
|genhide=
|crew=
|capacity=
|length m=9.75
|length ft=32
|length in=0
|span m=4.57
|span ft=15
|span in=0
|height m=2.29
|height ft=7
|height in=6
|wing area sqm=3.29
|wing area sqft=35.41
|empty weight kg=431
|empty weight lb=950
|gross weight kg=431
|gross weight lb=950
|eng1 number=
|eng1 type=
|eng2 number=
|eng2 type=
|perfhide=
|max speed kmh=277
|max speed mph=173
|stall speed kmh=111
|stall speed mph=69
|range km=18
|range miles=11
|ceiling m=3660
|ceiling ft=12000
|glide ratio=
|sink rate ms=
|sink rate ftmin=
}}

References

Notes

Bibliography

{{cite book |editor-last= Taylor|first= John W.R. |authorlink= |title= Jane's All the World's Aircraft 1973-74|year= 1973|publisher= Jane's Yearbooks |location=London, United Kingdom|isbn=0-354-00117-5}}

External links

NASA Hyper III photo collection and additional information

4 : Lifting bodies|United States experimental aircraft 1960–1969|NASA aircraft|Glider aircraft

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