XCOR EZ-Rocket: Difference between revisions
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* Two '''XR-4A3''' {{convert|400|lbf|kN|abbr=on}} thrust rocket engines (non throttleable, restartable in flight)<ref name=xcor-loxalc>{{cite web |url=http://xcor.com/engines/LOX-alcohol_4A3.html |title=LOX-Alcohol Rocket Engine |website=www.xcor.com |publisher=XCOR Aerospace, Inc. |access-date=2015-06-15 |url-status=dead |archive-url=https://web.archive.org/web/20150626025127/http://xcor.com/engines/LOX-alcohol_4A3.html |archive-date=2015-06-26 }}</ref> |
* Two '''XR-4A3''' {{convert|400|lbf|kN|abbr=on}} thrust rocket engines (non throttleable, restartable in flight)<ref name=xcor-loxalc>{{cite web |url=http://xcor.com/engines/LOX-alcohol_4A3.html |title=LOX-Alcohol Rocket Engine |website=www.xcor.com |publisher=XCOR Aerospace, Inc. |access-date=2015-06-15 |url-status=dead |archive-url=https://web.archive.org/web/20150626025127/http://xcor.com/engines/LOX-alcohol_4A3.html |archive-date=2015-06-26 }}</ref> |
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* 20 sec 500 m takeoff roll |
* 20 sec 500 m takeoff roll |
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* [[Overspeed (aeronautics)|Vne]] = 200 |
* [[Overspeed (aeronautics)|Vne]] = {{cvt|200|kn|km/h}} |
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* [[climb rate]] = 52 m/s (10,000 ft/min) |
* [[climb rate]] = 52 m/s (10,000 ft/min) |
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* maximum altitude = 11,546 |
* maximum altitude = {{cvt|11,546|ft|m}} MSL |
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* Fuel: isopropyl alcohol and liquid oxygen |
* Fuel: isopropyl alcohol and liquid oxygen |
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* Chamber pressure: ~ 350 |
* Chamber pressure: ~ {{cvt|350|psi|MPa}} |
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* [[Specific impulse]]: {{convert|250|isp}} to {{convert|270|isp}}{{Citation needed|date=July 2009}} |
* [[Specific impulse]]: {{convert|250|isp}} to {{convert|270|isp}}{{Citation needed|date=July 2009}} |
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* Noise: 128 dB at 10 meters<ref>{{cite web|url=http://www.xcor.com/products/vehicles/ez-rocket_faq.html |title=Archived copy |access-date=January 29, 2009 |url-status=dead |archive-url=https://web.archive.org/web/20090220232100/http://www.xcor.com/products/vehicles/ez-rocket_faq.html |archive-date=February 20, 2009 }}</ref> |
* Noise: 128 dB at 10 meters<ref>{{cite web|url=http://www.xcor.com/products/vehicles/ez-rocket_faq.html |title=Archived copy |access-date=January 29, 2009 |url-status=dead |archive-url=https://web.archive.org/web/20090220232100/http://www.xcor.com/products/vehicles/ez-rocket_faq.html |archive-date=February 20, 2009 }}</ref> |
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Revision as of 09:32, 31 July 2022
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
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
- October 8, 2000 - First firing of an XCOR Aerospace LOX-powered rocket engine.[3]
- July 21, 2001 - First flight, flown by Dick Rutan (single-engine configuration).[3]
- October 3, 2001 - First flight in twin-engine configuration.[3]
- January 24, 2002 - First rocketplane inflight engine relight. Piloted by Mike Melvill.
- June 24, 2002 - First touch-and-go of a rocket-powered aircraft (world record).[3]
- Jul 11, 2002 - EZ-Rocket flies twice in one day. First same day rocketplane flights since 1945.
- July 25, 2002 - EZ-Rocket first Oshkosh flight at the 2002 EAA AirVenture Oshkosh air show. First rocketplane air show flight in the United States.
- July 27, 2002 - EZ-Rocket second Oshkosh flight at the 2002 EAA AirVenture Oshkosh air show. Second rocketplane air show flight in the United States.
- August 26, 2005 - EZ-Rocket requalification flight after three-year retirement. Piloted by Dick Rutan.
- August 29, 2005 - Searfoss qualification flight.
- September 1, 2005 - Altitude validation flight to 11,546 feet. Aircraft demonstrated sufficient range to fly from Mojave to California City and back without a relight, a prerequisite for the world record flight.
- October 9, 2005 - EZ-Rocket second and third Las Cruces flights, at Countdown to X PRIZE Cup. Third and fourth rocketplane air show flights in the United States.
- December 3, 2005 - Set the point-to-point distance record for a ground-launched, rocket-powered aircraft, flying 16 km from Mojave to California City in just under ten minutes, piloted by Dick Rutan.[4][5] Also first official delivery of U.S. Mail by a rocket-powered aircraft.[4] In recognition of this achievement, the FAI awarded Rutan the 2005 Louis Blériot Medal.[6]
- December 15, 2005 - First cross-country return flight of a rocket-powered aircraft in the United States, return flight from California City, piloted by Rick Searfoss.[4]
Derivatives
The Rocket Racing League aircraft currently 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
- Two XR-4A3 400 lbf (1.8 kN) thrust rocket engines (non throttleable, restartable in flight)[7]
- 20 sec 500 m takeoff roll
- Vne = 200 kn (370 km/h)
- climb rate = 52 m/s (10,000 ft/min)
- maximum altitude = 11,546 ft (3,519 m) MSL
- Fuel: isopropyl alcohol and liquid oxygen
- Chamber pressure: ~ 350 psi (2.4 MPa)
- Specific impulse: 250 seconds (2.5 km/s) to 270 seconds (2.6 km/s)[citation needed]
- Noise: 128 dB at 10 meters[8]
See also
References
- ^ Flight Tests Of XCOR’s EZ-Rocket and Progress Toward a Microgravity and Microspacecraft Launcher
- ^ "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.
- ^ "Archived copy". Archived from the original on February 20, 2009. Retrieved January 29, 2009.
{{cite web}}: CS1 maint: archived copy as title (link)
External links
