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Innovative Comparison of Transient Ignition Temperature at the Booster Interface, New Stainless Steel Pyrovalve Primer Chamber Assembly "V" (PCA) Design Versus the Current Aluminum "Y" PCA DesignAn assessment of four spacecraft pyrovalve anomalies that occurred during ground testing was conducted by the NASA Engineering & Safety Center (NESC) in 2008. In all four cases, a common aluminum (Al) primer chamber assembly (PCA) was used with dual NASA Standard Initiators (NSIs) and the nearly simultaneous (separated by less than 80 microseconds) firing of both initiators failed to ignite the booster charge. The results of the assessment and associated test program were reported in AIAA Paper AIAA-2008-4798, NESC Independent Assessment of Pyrovalve Ground Test Anomalies. As a result of the four Al PCA anomalies, and the test results and findings of the NESC assessment, the Mars Science Laboratory (MSL) project team decided to make changes to the PCA. The material for the PCA body was changed from aluminum (Al) to stainless steel (SS) to avoid melting, distortion, and potential leakage of the NSI flow passages when the device functioned. The flow passages, which were interconnected in a Y-shaped configuration (Y-PCA) in the original design, were changed to a V-shaped configuration (V-PCA). The V-shape was used to more efficiently transfer energy from the NSIs to the booster. Development and qualification testing of the new design clearly demonstrated faster booster ignition times compared to the legacy AL Y-PCA design. However, the final NESC assessment report recommended that the SS V-PCA be experimentally characterized and quantitatively compared to the Al Y-PCA design. This data was deemed important for properly evaluating the design options for future NASA projects. This test program has successfully quantified the improvement of the SS V-PCA over the Al Y-PCA. A phase B of the project was also conducted and evaluated the effect of firing command skew and enlargement of flame channels to further assist spacecraft applications.
Document ID
20110014013
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Saulsberry, Regor L.
(NASA White Sands Test Facility NM, United States)
McDougle, Stephen H.
(NASA White Sands Test Facility NM, United States)
Garcia,Roberto
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Johnson, Kenneth L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Sipes, William
(Sipes (William) Canyon Country, CA, United States)
Rickman, Steven
(NASA Johnson Space Center Houston, TX, United States)
Hosangadi, Ashvin
(Combustion Research and Flow Technology, Inc. Pipersville, PA, United States)
Date Acquired
August 25, 2013
Publication Date
July 31, 2011
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JSC-CN-24274
Meeting Information
Meeting: 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Location: San Diego, CA
Country: United States
Start Date: July 31, 2011
End Date: August 3, 2011
Sponsors: American Society of Mechanical Engineers, American Inst. of Aeronautics and Astronautics, American Society for Electrical Engineers, Society of Automotive Engineers, Inc.
Distribution Limits
Public
Copyright
Public Use Permitted.
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