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Augmented orbiter heat rejection study
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hixon, C. W. |
| Copyright Year | 1981 |
| Description | Spacecraft radiator concepts are presented that relieve attitude restrictions required by the shuttle orbiter space radiator for baseline and extended capability STS missions. Cost effective heat rejection kits are considered which add additional capability in the form of attached spacelab radiators or a deployable radiator module. |
| File Size | 23360917 |
| Page Count | 132 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810016600 |
| Archival Resource Key | ark:/13960/t2n63c672 |
| Language | English |
| Publisher Date | 1981-02-18 |
| Access Restriction | Open |
| Subject Keyword | Space Transportation Attitude Inclination Spacelab Cost Effectiveness Spacecraft Radiators Cooling Systems Space Transportation System Space Shuttle Orbiters Radiative Heat Transfer Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |