| タイトル | Selection process for trade study: Graphite Composite Primary Structure (GCPS) |
| 本文（外部サイト） | http://hdl.handle.net/2060/19950005390 |
| 著者（英） | Greenberg, H. S. |
| 著者所属（英） | Rockwell International Corp.; Grumman Aerospace Corp. |
| 発行日 | 1994-09-02 |
| 言語 | eng |
| 内容記述 | This TA 2 document describes the selection process that will be used to identify the most suitable structural configuration for an SSTO winged vehicle capable of delivering 25,000 lbs to a 220 nm circular orbit at 51.6 degree inclination. The most suitable unpressurized graphite composite structures and material selections is within this configuration and will be the prototype design for subsequent design and analysis and the basis for the design and fabrication of payload bay, wing, and thrust structure full scale test articles representing segments of the prototype structures. The selection process for this TA 2 trade study is the same as that for the TA 1 trade study. As the trade study progresses additional insight may result in modifications to the selection criteria within this process. Such modifications will result in an update of this document as appropriate. |
| NASA分類 | COMPOSITE MATERIALS |
| レポートNO | 95N11803
NASA-CR-196866
NAS 1.26:196866
SSD94D0210 |
| 権利 | No Copyright |
