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Contents

   



(Top)
 


1 Development and history  





2 Milestones and records  





3 Derivatives  





4 Specifications  





5 See also  





6 References  





7 External links  














XCOR EZ-Rocket







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From Wikipedia, the free encyclopedia
 

(Redirected from XCOR EZRocket)

EZ-Rocket one week after its first flight
Cockpit. Engine on-off switches on left side panel are placarded "FWD - LOUD; BACK - QUIET"

The XCOR EZ-Rocket was a test platform for the XCOR XR-4A3 rocket propulsion system. The airplane was a modified Rutan Long-EZ, with the propeller replaced by first one, then later a pair of pressure-fed regeneratively cooled liquid-fueled rocket engines and an underslung fuel tank. The engines were restartable in flight, and were contained within Kevlar armor shielding. The EZ-Rocket was registered as an experimental aircraft.

Development and history[edit]

The first flight took place on July 21, 2001, flown by test pilot Dick Rutan.[1]

On a typical flight, the EZ-Rocket took off on rockets, gained altitude for a minute or so, then switched off the rockets and glided to a dead stick landing.

The vehicle actually flew better during dead stick landings than a standard Long-EZ due to lack of drag from a stationary pusher propeller — the vehicle's aerodynamics were cleaner in spite of its belly tank. It was also lighter due to the lack of a piston engine (the rocket propulsion system was significantly lighter), so enjoyed significantly lower wing loading than a standard Long-EZ.

When XCOR began flying its EZ-Rocket in 2001, the company decided to have it FAA certified as an experimental aircraft, avoiding the additional time required to seek a launch vehicle license from the Office of Commercial Space Transportation (AST). Jeff Greason, a co-founder of XCOR, said on February 10, 2003 if they were starting out at that time they probably would seek an AST license due to the progress made in developing a regulatory regime for suborbitals.[2]

Milestones and records[edit]

EZ-Rocket, flown by Dick Rutan, touches down at California City, California on December 3, 2005, setting a point-to-point distance record for rocket-powered, ground-launched aircraft.

Derivatives[edit]

The Rocket Racing League aircraft currently[when?] in development, the Mark-III X-racer, is a design descendant of the EZ-Rocket aircraft. Although XCOR is not the developer of the rocket engine for the Mark-III, XCOR did develop the rocket engine for the Mark-I X-Racer, the first of the X-Racers to use a single rocket engine on a Velocity SE basic airframe, and the first X-Racer to utilize kerosene instead of isopropyl alcohol fuel. XCOR used both design and operational experience from the EZ-Rocket in the Mark-I rocket aircraft design.[citation needed]

Specifications[edit]

Twin rocket engines
Dick Rutan standing next to the engines of the EZ-Rocket, after the official rollout flight, November 12, 2001

See also[edit]

References[edit]

  • ^ "Reusable Launch Vehicle (RLV) News". HobbySpace. Retrieved 2022-05-02.
  • ^ a b c d "First Flights — XCOR Aerospace". Mojave Virtual Museum. Archived from the original on 2006-11-10. Retrieved 2006-11-13.
  • ^ a b c Deaver, Bill (2005-12-22). "XCOR EZ-Rocket makes more history at CalCity". Mojave Desert News.
  • ^ FAI Records Archived March 10, 2007, at the Wayback Machine
  • ^ List of Blériot medals awarded to Dick Rutan[permanent dead link]
  • ^ "LOX-Alcohol Rocket Engine". www.xcor.com. XCOR Aerospace, Inc. Archived from the original on 2015-06-26. Retrieved 2015-06-15.
  • ^ "XCOR Aerospace: EZ-Rocket FAQ". Archived from the original on February 20, 2009. Retrieved January 29, 2009.
  • External links[edit]


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