A "pad abort" flight test of the Max Launch Abort System was performed at NASA's Wallops Flight Facility on July 8, 2009, at 10:26 UTC.1112 A primary test goal was the successful separation of a mock crew capsule from the abort system.13 The test vehicle weighed over 45,000 pounds (20,000 kg) and was over 33 feet (10 m) tall.14
The test vehicle had several differences from the actual proposed system. The main difference was that the four propulsion rockets were not located in the forward fairing, but in a boost skirt located at the bottom of the test vehicle.15 The rockets in the fairing were represented by geometric dummies.16 The propulsion thrust was not balanced between the rockets by a manifold system, contrary to what was foreseen with the actual system.17
This article incorporates public domain material from websites or documents of the National Aeronautics and Space Administration.
Media related to Max Launch Abort System at Wikimedia Commons
"NASA's Max Launch Abort System (MLAS) Overview". NASA. Retrieved August 15, 2024. https://www.nasa.gov/exploration/features/MLAS_overview.html ↩
"NASA Considering Alternate Launch Abort System for Orion". NASASpaceFlight.com. December 6, 2007. Retrieved August 15, 2024. https://www.nasaspaceflight.com/2007/12/nasa-considering-alternate-launch-abort-system-for-orion/ ↩
"NASA's Constellation Program: Max Launch Abort System". NASA. Retrieved August 15, 2024. https://www.nasa.gov/mission_pages/constellation/main/index.html ↩
"Max Q: The Ultimate Challenge of Space Flight". NASA. October 29, 2019. Retrieved August 15, 2024. https://www.nasa.gov/feature/max-q-the-ultimate-challenge-of-space-flight ↩
"NASA's Wallops Flight Facility and the MLAS". NASA/Wallops Flight Facility. July 1, 2009. Retrieved August 15, 2024. https://www.nasa.gov/centers/wallops/news/feature10.html ↩
Isakowitz, Steven J. (2010). International Reference Guide to Space Launch Systems. AIAA. pp. 357–359. ISBN 978-1-60086-784-2. 978-1-60086-784-2 ↩
Wood, Eric M. (2010). "Reliability Considerations of Multiple Solid Rocket Motors in Launch Abort Systems". Journal of Spacecraft and Rockets. 47 (2): 317–321. doi:10.2514/1.47414 (inactive 1 November 2024).{{cite journal}}: CS1 maint: DOI inactive as of November 2024 (link) /wiki/Doi_(identifier) ↩
Connors, Mary M. (2008). Launch Escape Systems and Emergency Recovery: Historical Overview and Future Prospects. NASA. pp. 112–115. ↩
Shayler, David (2001). Gemini: Steps to the Moon. Springer-Praxis. pp. 192–194. ISBN 978-1-85233-405-5. 978-1-85233-405-5 ↩
Garcia, Mark (15 January 2015). "NASA's Orion Multi-Purpose Crew Vehicle (MPCV)". NASA. Retrieved August 15, 2024. https://www.nasa.gov/exploration/systems/mpcv/index.html ↩
Hautaluoma, Grey; Edwards, Ashley; Henry, Keith; Powell, Rebecca (July 8, 2009). "NASA Tests Alternate Launch Abort System For Astronaut Escape". NASA. NASA Release 09-156. https://www.nasa.gov/home/hqnews/2009/jul/HQ09_156_MLAS_launch_successful.html ↩
"Max Launch Abort System (MLAS)". NASA. July 8, 2009. https://www.nasa.gov/exploration/multimedia/galleries/mlas-13.html ↩
"MLAS". NASA/Wallops Flight Facility. Retrieved July 11, 2009. https://www.nasa.gov/centers/wallops/missions/mlas.html ↩