Author : National Aeronautics and Space Adm Nasa
Publisher : Independently Published
ISBN 13 : 9781793956736
Total Pages : 36 pages
Book Rating : 4.9/5 (567 download)
Book Synopsis Guidance, Navigation and Control (Gn and C) Design Overview and Flight Test Results from Nasa's Max Launch Abort System (Mlas) by : National Aeronautics and Space Adm Nasa
Download or read book Guidance, Navigation and Control (Gn and C) Design Overview and Flight Test Results from Nasa's Max Launch Abort System (Mlas) written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2019-01-14 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: The National Aeronautics and Space Administration Engineering and Safety Center designed, developed and flew the alternative Max Launch Abort System (MLAS) as risk mitigation for the baseline Orion spacecraft launch abort system already in development. The NESC was tasked with both formulating a conceptual objective system design of this alternative MLAS as well as demonstrating this concept with a simulated pad abort flight test. Less than 2 years after Project start the MLAS simulated pad abort flight test was successfully conducted from Wallops Island on July 8, 2009. The entire flight test duration was 88 seconds during which time multiple staging events were performed and nine separate critically timed parachute deployments occurred as scheduled. This paper provides an overview of the guidance navigation and control technical approaches employed on this rapid prototyping activity; describes the methodology used to design the MLAS flight test vehicle; and lessons that were learned during this rapid prototyping project are also summarized. Dennehy, Cornelius J. and Lanzi, Raymond J. and Ward, Philip R. Goddard Space Flight Center; Langley Research Center; Wallops Flight Facility NASA/TM-2010-216877, L-19963, NF1676L-11924