. | . |
Antares rocket engine failure causes by Staff Writers Bethesda MD (SPX) Nov 05, 2015
Just three weeks ago, NASA's Independent Review Team released the Executive Summary of its Orb-3 Accident Investigation Report. This report chronicles the events and summarizes the likely failure causes associated with the October 28, 2014 launch of the Orbital ATK Orb-3 cargo resupply mission to the ISS. The Orb-3 vehicle consisted of an Antares-130 launch vehicle plus a standard Cygnus spacecraft. The payload was 2,300 kg of pressurized cargo . This was Orbital ATK's third cargo mission under its ISS CRS contract. Just over 15 seconds into flight an explosion in the Antares Main Engine System occurred. This event caused the vehicle to lose thrust and fall back toward the ground in close proximity to the launch pad. There was a complete loss of the vehicle and cargo. While there was some damage to the launch pad facilities, there were no injuries. The Independent Review Team (IRT) was formed in November 2014 to determine the technical root cause of the Orb-3 failure and make recommendations leading to more reliable systems. A detailed review and analysis of telemetry, photographs and video media led to the likely conclusion that the mission failed due to an explosion in the AJ26 rocket engine installed in the Engine 1 position. Apparently, there was an explosion in the E15 liquid oxygen turbopump, which then damaged the rocket engine installed in the Engine 2 position. Thus, both engines lost thrust and the vehicle fell back to Earth. Although the IRT was not able to isolate a single technical root cause for the engine fire and explosion, three credible technical root causes were identified, any one, or a combination, of which could have resulted in the failure: 1.Inadequate design robustness of the AJ26 liquid oxygen turbopump Hydraulic Balance Assembly and turbine-end bearing for Antares; 2.Foreign Object Debris introduction to the liquid oxygen turbopump; 3.Manufacturing or other workmanship defect in the liquid oxygen turbopump. In conclusion, the IRT report dictated that all three of these technical root causes need to be addressed as part of any return to flight efforts for Antares. The complete Executive Summary is available here
Related Links Launchspace Rocket Science News at Space-Travel.Com
|
|
The content herein, unless otherwise known to be public domain, are Copyright 1995-2024 - Space Media Network. All websites are published in Australia and are solely subject to Australian law and governed by Fair Use principals for news reporting and research purposes. AFP, UPI and IANS news wire stories are copyright Agence France-Presse, United Press International and Indo-Asia News Service. ESA news reports are copyright European Space Agency. All NASA sourced material is public domain. Additional copyrights may apply in whole or part to other bona fide parties. All articles labeled "by Staff Writers" include reports supplied to Space Media Network by industry news wires, PR agencies, corporate press officers and the like. Such articles are individually curated and edited by Space Media Network staff on the basis of the report's information value to our industry and professional readership. Advertising does not imply endorsement, agreement or approval of any opinions, statements or information provided by Space Media Network on any Web page published or hosted by Space Media Network. General Data Protection Regulation (GDPR) Statement Our advertisers use various cookies and the like to deliver the best ad banner available at one time. All network advertising suppliers have GDPR policies (Legitimate Interest) that conform with EU regulations for data collection. By using our websites you consent to cookie based advertising. If you do not agree with this then you must stop using the websites from May 25, 2018. Privacy Statement. Additional information can be found here at About Us. |