| タイトル | Shuttle payload interface verification equipment study. Volume 1: Executive summary |
| 本文（外部サイト） | http://hdl.handle.net/2060/19760015173 |
| 著者所属（英） | Rockwell International Corp. |
| 発行日 | 1976-04-01 |
| 言語 | eng |
| 内容記述 | A preliminary design analysis of a stand alone payload integration device (IVE) is provided that is capable of verifying payload compatibility in form, fit and function with the shuttle orbiter prior to on-line payload/orbiter operations. The IVE is a high fidelity replica of the orbiter payload accommodations capable of supporting payload functional checkout and mission simulation. A top level payload integration analysis developed detailed functional flow block diagrams of the payload integration process for the broad spectrum of P/L's and identified degree of orbiter data required by the payload user and potential applications of the IVE. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 76N22261
SD76-SH-0092-VOL-1
NASA-CR-147665 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/186165 |
