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Orion Boiler Plate Airdrop Test SystemOn the 29th of February 2012 the Orion Capsule Parachute Assembly System (CPAS) project attempted to perform an airdrop test of a boilerplate test article for the second time. The first attempt (Cluster Development Test 2, July 2008) to deliver a similar boilerplate from a C-17 using the Low Velocity Air Drop (LVAD) technique resulted in the programmer parachute failing to properly inflate, the test article failing to achieve the desired test initiation conditions, and the test article a total loss. This paper will pick up where the CDT-2 failure investigation left off, describing the test technique that was adopted, and outline the modeling that was performed to gain confidence that the second attempt would be successful. The second boiler plate test (Cluster Development Test 3-3) was indeed a complete success and has subsequently been repeated several times, allowing the CPAS project to proceed with the full scale system level development testing required to integrate the hardware to the first Entry Flight Test vehicle as well as go into the Critical Design Review with minimum risk and a mature design.
Document ID
20130011424
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Machin, Ricardo A.
(NASA Johnson Space Center Houston, TX, United States)
Evans, Carol T.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 27, 2013
Publication Date
March 25, 2013
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
JSC-CN-27860
Report Number: JSC-CN-27860
Meeting Information
Meeting: 22nd AIAA Aerodynamic Decelerator Systems
Location: Daytona Beach, FL
Country: United States
Start Date: March 25, 2013
End Date: March 28, 2013
Funding Number(s)
WBS: WBS 747797.06.14.03.99.10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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