درباره ما
NASA-LLIS-0572
Lessons Learned – Damage to Bipropellant Main Engines from Premature Oxidizer Depletion (1997)
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:07:46Z | |
| date available | 2017-09-04T16:07:46Z | |
| date copyright | 07/17/1997 | |
| date issued | 1997 | |
| identifier other | SCCEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/70942 | |
| description abstract | Abstract: Premature depletion of one propellant can occur in bipropellant systems if engine and component acceptance test data are not properly considered when determining the flight propellant loads. Oxidizer depletion may be difficult to detect from accelerometer readings. The lesson suggests methods for (1) determining flight propellant loads and consumption and (2) determining the onset of oxidizer depletion and triggering burn termination. | |
| language | English | |
| title | NASA-LLIS-0572 | num |
| title | Lessons Learned – Damage to Bipropellant Main Engines from Premature Oxidizer Depletion (1997) | en |
| type | standard | |
| page | 3 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1997 | |
| contenttype | fulltext | |
| subject keywords | Engine Flow Test Data |
