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The apollo 15 deployable boom anomaly
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | White, R. D. |
| Copyright Year | 1972 |
| Description | During the Apollo 15 mission, a boom with an attached mass spectrometer was required to retract periodically so that the instrument would not be in the field of view of other experiments. The boom did not fully retract on five of 12 occasions. Data analysis indicated that the boom probably retracted to within approximately 2.54 centimeters (1 inch) of full retraction. The pertinent boom-design details, the events in the mission related to the anomaly, a discussion of the inflight and postflight investigation of the problem, a discussion of the design changes to the boom mechanism as a result of the investigation, and subsequent flight performance are presented. |
| File Size | 1763211 |
| Page Count | 12 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730010141 |
| Archival Resource Key | ark:/13960/t5k97z96q |
| Language | English |
| Publisher Date | 1972-11-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles System Failures Space Erectable Structures Spectrometers Failure Analysis Booms Equipment Apollo 15 Flight Experiment Design Spacecraft Structures Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
