درباره ما
NASA-LLIS-1491
Lessons Learned – Thorough Risk Assessment in the Design Phase
Year: 2004
Abstract: Abstract:
In November of 2003, the NASA Engineering and Safety 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 d'Etudes Spatiales (CNES) scheduled to launch from Vandenberg Air Force base in April 2005 on a Delta II rocket. Several personnel safety hazards related to the hydrazine-fueled Proteus propulsion bus could have been minimized or avoided in the design phase.
In November of 2003, the NASA Engineering and Safety 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 d'Etudes Spatiales (CNES) scheduled to launch from Vandenberg Air Force base in April 2005 on a Delta II rocket. Several personnel safety hazards related to the hydrazine-fueled Proteus propulsion bus could have been minimized or avoided in the design phase.
Subject: Flight Equipment
Show full item record
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:08:40Z | |
| date available | 2017-09-04T17:08:40Z | |
| date copyright | 04/26/2004 | |
| date issued | 2004 | |
| identifier other | YKWEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/132140 | |
| description abstract | Abstract: In November of 2003, the NASA Engineering and Safety 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 d'Etudes Spatiales (CNES) scheduled to launch from Vandenberg Air Force base in April 2005 on a Delta II rocket. Several personnel safety hazards related to the hydrazine-fueled Proteus propulsion bus could have been minimized or avoided in the design phase. | |
| language | English | |
| title | NASA-LLIS-1491 | num |
| title | Lessons Learned – Thorough Risk Assessment in the Design Phase | en |
| type | standard | |
| page | 3 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2004 | |
| contenttype | fulltext | |
| subject keywords | Flight Equipment | |
| subject keywords | Ground Operations | |
| subject keywords | NASA Standards | |
| subject keywords | Program and Project Management | |
| subject keywords | Range Operations | |
| subject keywords | Risk Management/Assessment | |
| subject keywords | Spacecraft |