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Max Launch Abort System (MLAS) Landing Parachute Demonstrator (LPD) Drop TestThe Landing Parachute Demonstrator (LPD) was conceived as a low-cost, rapidly-developed means of providing soft landing for the Max Launch Abort System (MLAS) crew module (CM). Its experimental main parachute cluster deployment technique and off-the-shelf hardware necessitated a full-scale drop test prior to the MLAS mission in order to reduce overall mission risk. This test was successfully conducted at Wallops Flight Facility on March 6, 2009, with all vehicle and parachute systems functioning as planned. The results of the drop test successfully qualified the LPD system for the MLAS flight test. This document captures the design, concept of operations and results of the drop test.
Document ID
20110011505
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Shreves, Christopher M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 25, 2013
Publication Date
May 1, 2011
Subject Category
Space Transportation And Safety
Report/Patent Number
L-20023
NASA/TM-2011-217086
NF1676L-12643
Report Number: L-20023
Report Number: NASA/TM-2011-217086
Report Number: NF1676L-12643
Funding Number(s)
WBS: WBS 869021.05.07.07.10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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