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XCOR EZ-Rocket : ウィキペディア英語版
XCOR EZ-Rocket

The XCOR EZ-Rocket is a test platform for the XCOR rocket propulsion system. The airplane is a modified Rutan Long-EZ, with the propeller replaced by first one, then later a pair of pressure-fed regeneratively cooled liquid-fuelled rocket engines and an underslung fuel tank. The engines are restartable in flight, and are contained within Kevlar armor shielding. The EZ-Rocket is registered as an experimental aircraft.
==Development and history==
The first flight took place on July 21, 2001, flown by test pilot Dick Rutan.
On a typical flight, the EZ-Rocket takes off on rockets, gains altitude for a minute or so, then switches off the rockets and glides to a deadstick landing.
The vehicle actually flies better during deadstick glide landings than a Long-EZ due to lack of drag from a stationary pusher propeller — the vehicle's aerodynamics are cleaner in spite of its belly tank. It is also lighter due to the lack of a piston engine (the rocket propulsion system is significantly lighter), so enjoys significantly lower wing loading than a stock Long-EZ.
XCOR registered it as a conventional aircraft, rather than a suborbital, because the vehicle is incapable of reaching the 100 km Kármán line altitude.

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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