| タイトル | Orbiter wheel and tire certification |
| 本文（外部サイト） | http://hdl.handle.net/2060/19850008650 |
| 著者（英） | Campbell, C. C., Jr. |
| 著者所属（英） | NASA Johnson Space Center |
| 発行日 | 1985-01-01 |
| 言語 | eng |
| 内容記述 | The orbiter wheel and tire development has required a unique series of certification tests to demonstrate the ability of the hardware to meet severe performance requirements. Early tests of the main landing gear wheel using conventional slow roll testing resulted in hardware failures. This resulted in a need to conduct high velocity tests with crosswind effects for assurance that the hardware was safe for a limited number of flights. Currently, this approach and the conventional slow roll and static tests are used to certify the wheel/tire assembly for operational use. |
| NASA分類 | SPACE TRANSPORTATION |
| レポートNO | 85N16959 |
| 権利 | No Copyright |
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