J-2X

J-2X

A CGI artist's impression of a J-2X.Spa
Country of origin United States
Manufacturer Aerojet Rocketdyne
Application Upper stage engine
Associated L/V Block II Space Launch System (EDS)
Predecessor J-2
Status Cancelled
Liquid-fuel engine
Propellant Liquid oxygen / Liquid hydrogen
Mixture ratio 5.5-4.5
Cycle Gas generator
Configuration
Nozzle ratio 92:1
Performance
Thrust (vac.) 1,307 kN (294,000 lbf)
Thrust-to-weight ratio 55.04
Isp (vac.) 448 seconds (4.39 km/s)
Dimensions
Length 4.7 metres (15 ft)
Diameter 3 metres (9.8 ft)
Dry weight 5,450 pounds (2,470 kg)
References
References [1][2]

The J-2X is a liquid-fueled cryogenic rocket engine that was planned for use on the Ares rockets of NASA's Constellation program, and later the Space Launch System. Built in the United States by Aerojet Rocketdyne (formerly, Pratt & Whitney Rocketdyne), the J-2X burns cryogenic liquid hydrogen & liquid oxygen propellants, with each engine producing 1,307 kN (294,000 lbf) of thrust in vacuum at a specific impulse (Isp) of 448 seconds (4.39 km/s).[2] The engine's mass is approximately 2,470 kg (5,450 Lb), significantly heavier than its predecessors.[2]

The J-2X was intended to be based on the J-2 used on the S-II and S-IVB stages of the Saturn rockets used during the Apollo program, but as required thrust for the Ares I increased due to weight problems it became a clean sheet design. It entered development in 2007 as part of the cancelled Constellation program.[2] Originally planned for use on the upper stages of the Ares I and Ares V rockets, the J-2X was later intended for use in the Earth Departure Stage of the Block II Space Launch System, the successor to the Constellation program. The engine is intended to be more efficient and simpler to build than its J-2 ancestor, and cost less than the RS-25 Space Shuttle Main Engine.[1] Differences in the new engine include the removal of beryllium, a centrifugal turbo pump versus the axial turbo pump of the J-2, different chamber and nozzle expansion ratios, a channel-walled combustion chamber versus the tube-welded chamber of the J-2, a redesign of all the electronics, a gas generator and supersonic main injector based on the RS-68,[3] and the use of 21st-century joining techniques.[2][4]

Testing

On 16 July 2007 NASA officially announced the award to Pratt & Whitney Rocketdyne (PWR) of a $1.2 billion contract "for design, development, testing and evaluation of the J-2X engine",[5] and began construction of a new test stand for altitude testing of J-2X engines at Stennis Space Center on 23 August 2007.[6]

Component testing was undertaken between December 2007 and May 2008, with nine tests of heritage J-2 engine components at SSC in preparation for the design of the J-2X engine.[7] and on 8 September 2008 PWR announced successful testing of the initial J-2X gas generator design.[8] The completion of a second round of successful gas generator tests was announced on 21 September 2010.[9]

Starting in 2011, the full J-2X engine, derived from heritage and new designs, has undergone hot-fire tests.

Program status

In October 2013, it was reported that work on the J-2X would pause following development testing in 2014, due to funding limitations, an expected delayed need for the engine's capabilities for piloted missions to Mars, and selection[18] of the RL10 powered Exploration Upper Stage for SLS.[19]

See also

Aerojet Rocketdyne J-2X Engine

References

Wikimedia Commons has media related to J-2X (rocket engine).
  1. 1 2 "J-2X Engine". Aerojet Rocketdyne. Retrieved 9 January 2014.
  2. 1 2 3 4 5 Mark Wade (17 November 2011). "J-2X". Encyclopedia Astronautica.
  3. ↑ "The J-2X Upper Stage Engine: From Design to Hardware. Thomas Byrd, Deputy Manager, J-2X Upper Stage Engine Element Ares Projects Office Marshall Space Flight Center Huntsville, AL 35812" (PDF).
  4. ↑ William D Greene (4 June 2012). "J-2X Extra: What's in a Name?". NASA.
  5. ↑ "NASA Awards Upper Stage Engine Contract for Ares Rockets". NASA. 16 July 2007. Retrieved 17 July 2007.
  6. ↑ "NASA's Stennis Space Center Marks New Chapter in Space Exploration". NASA. 23 August 2007.
  7. ↑ "NASA Successfully Completes First Series of Ares Engine Tests". NASA. 8 May 2008.
  8. ↑ "Pratt & Whitney Rocketdyne Completes Successful Test of J-2X Gas Generator". Pratt & Whitney Rocketdyne. 8 September 2008.
  9. ↑ "Pratt & Whitney Rocketdyne Completes Latest Round of Tests on J-2X Gas Generator" (Press release). Pratt & Whitney Rocketdyne. September 21, 2010.
  10. ↑ Morring, Frank. "First J-2X Hot-Fire Test Could Come Next Week". Aviation Week. Retrieved 19 June 2011.
  11. ↑ "NASA Test Fires Engine for Giant New Rocket". Space.com. 9 November 2011. Retrieved 26 February 2012.
  12. ↑ "NASA Surpasses Test Facility Record with J-2X Powerpack Test". National Aeronautics and Space Administration. 8 June 2012. Retrieved 10 June 2012.
  13. ↑ "A Summer of Records for Engine Testing". National Aeronautics and Space Administration. 26 June 2012. Retrieved 26 June 2012.
  14. ↑ "Beating Heart of J-2X Engine Finishes Year of Successful Testing". National Aeronautics and Space Administration. 13 Dec 2012. Retrieved 14 Dec 2012.
  15. ↑ "NASA Set for New Round Of J-2X Testing at Stennis Space Center". National Aeronautics and Space Administration. 11 Feb 2013. Retrieved 6 Feb 2014.
  16. 1 2 "J-2X Progress: November 2013 Update". National Aeronautics and Space Administration. 15 Nov 2013. Retrieved 6 Feb 2014.
  17. ↑ "One Final Test for J-2X Engine No. 10002". National Aeronautics and Space Administration. 5 Sep 2013. Retrieved 6 Feb 2014.
  18. ↑ Bergin, Chris. "NASA lines up Exploration Upper Stage workhorse for SLS". NASASpaceflight.com. Retrieved November 8, 2014.
  19. ↑ "NASA's J-2X Engine To Be Mothballed After Testing". Aviation Week and Space Technology magazine. 4 Oct 2013. Retrieved 29 Oct 2013.
This article is issued from Wikipedia - version of the 11/27/2016. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.