| 词条 | Kaman KSA-100 SAVER | |||||||||||||||||
| 释义 |
The Kaman KSA-100 SAVER (Stowable Aircrew Vehicle Escape Rotorseat) is an American aircraft-stowable gyroplane escape device designed and built by the Kaman Aerospace Corporation for the United States Navy. Designed to be used in naval combat aircraft to deploy as part of the ejection sequence, only one was built and it did not enter service. It was the first jet-powered gyroplane. Design and developmentThe United States Navy Air Development Center awarded a number of contracts to aerospace companies to find a method for ejected aircrew to escape from the scene of the crash. Kaman proposed a turbofan powered gyroplane it called the Stowable Aircrew Vehicle Escape Rotorseat or SAVER, it was a gyroplane with an unpowered rotor, the blades being telescopic and along with the turbofan engine would fold into the aircraft seat during normal use. When the pilot ejected the seat would leave the aircraft and a drogue parachute would slow the seat and deploy the blades within four seconds. After an additional two seconds, the turbofan would run up to full power and the seat would become a gyroplane. Kaman made over 1500 air drops to test the self-deploying rotor system and a full-scale unpowered SAVER was tested by NASA in the Ames Research Laboraatory wind tunnel in 1970. The SAVER was equipped with a ground handling frame for tests, which was a tricycle landing gear and support frame, also fitted with basic flight instruments. The SAVER first flew in a towed flight on 28 December 1971 and the following day made a free flight, although it was fitted with a 16 ft non-telescoping rotor. Fitted with the 14 ft telescopic rotor, it first flew 10 January 1972. The SAVER was fitted with a Williams WRC-19 turbofan which was too powerful for the seat but was available "off the shelf." The program was to test the seat unmanned in an air launch but the program was cancelled as the military did not think the idea was a viable proposition. The SAVER was an aircraft ejection seat with a Williams WRC-19 turbofan engine and a two-bladed non-powered rotor attached to the seat structure. It had a parachute in the headrest assembly and a seat back fitted with a life raft and survival gear. Specifications{{aerospecs|ref=Jane's All the World's Aircraft 1973-74 |met or eng?=eng |genhide= |crew=one |capacity= |length m= |length ft= |length in= |rot number=1 |rot dia m=4.27 |rot dia ft=14 |rot dia in=0 |height m= |height ft= |height in= |rot area sqm= |rot area sqft= |empty weight kg=201 |empty weight lb=444 |gross weight kg=322 |gross weight lb=710 |eng1 number=1 |eng1 type=Williams WRC-19 turbofan engine |eng1 kn=1.91 |eng1 lbf=430 |eng2 number= |eng2 type= |perfhide= |max speed kmh=185 |max speed mph=115 |range km=92 |range miles=57 |ceiling m= |ceiling ft= |climb rate ms= |climb rate ftmin= }}{{aircontent |see also= |related= |similar aircraft= |sequence= |lists=
}} References{{commons category|Kaman helicopters}}
7 : United States experimental aircraft 1970–1979|Kaman aircraft|Autogyros|Pusher aircraft|Single-engined jet aircraft|Aircraft emergency systems|Ejection seats |
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