NASA-LLIS-0305
Lessons Learned – Galileo Retro Propulsion Module (RPM) Flow Decay Problem
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:11:22Z | |
| date available | 2017-09-04T16:11:22Z | |
| date copyright | 09/01/1993 | |
| date issued | 1993 | |
| identifier other | SMAEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/74600 | |
| description abstract | Abstract: To reduce costs, the Mars Observer propulsion and other subsystems followed design practices more common to earth-orbiting satellites than to planetary missions. Consider contractor experience in bipropellant spacecraft propulsion system design in source selection. To manage risk on one-of-akind developments, assure thorough technical oversight of contractors with limited experience in the design of interplanetary spacecraft. | |
| language | English | |
| title | NASA-LLIS-0305 | num |
| title | Lessons Learned – Galileo Retro Propulsion Module (RPM) Flow Decay Problem | en |
| type | standard | |
| page | 2 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1993 | |
| contenttype | fulltext | |
| subject keywords | Parts Materials & Processes | |
| subject keywords | Spacecraft |

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