REG NASA-LLIS-1492--2004 Lessons Learned - Standards Specifications and Processes for Projects with Outside Partners.pdf
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1、Lessons Learned Entry: 1492Lesson Info:a71 Lesson Number: 1492a71 Lesson Date: 2004-04-27a71 Submitting Organization: LARCa71 Submitted by: Richard J. GilbrechSubject: Standards, Specifications and Processes for Projects with Outside Partners Abstract: In November of 2003, the NASA Engineering and S
2、afety Center (NESC) performed an Independent Technical Assessment of the Code Y CALIPSO satellite Proteus propulsion bus (ref. NESC Final Report NESC-RP-001, NASA Technical Memorandum number applied for). This is a joint mission with NASA GSFC, LaRC and the Centre National dEtudes Spatiales (CNES) s
3、cheduled to launch from Vandenberg Air Force base in April 2005 on a Delta II rocket. There was a high level of confusion among the partners as to what standards, specifications and processes were to be applied (i.e., NASA, French, or DOD).Description of Driving Event: The CALIPSO program involved N
4、ASA GSFC, LaRC, KSC Launch Services, CNES, and the Vandenberg Air Force Base Range Office. CNES contributed the Proteus hydrazine-fueled propulsion bus as part of their in-kind contribution. This bus was designed and built by Alcatel Space Industries under subcontract to CNES. The Memorandum of Unde
5、rstanding (MOU) between NASA and CNES placed the responsibility for design of the propulsion bus with CNES yet did not explicitly state which safety requirements applied. Several personnel hazards associated with the Proteus bus formed the basis of the NESC assessment (leakage of hydrazine from thre
6、aded A/N fittings, inadvertent thruster firings and leakage of hydrazine through the thrusters). It was accepted by all that the Air Force Eastern and Western Range (EWR) requirements applied (ref. CALIPSO-Tailored Eastern and Western Range 127-1 Safety Regulations, Doc. TP2.LB.0.AQ.1836 ASC dated O
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