发明名称 |
Aerospace vehicle |
摘要 |
A dual structure aerospace vehicle 10 having an aeroshell structure 11 and an internally disposed separable and reusable integral tank/thrust structure 13 is disclosed. Tank/thrust structure 13 is insulated for cryogenic fuels and the cavity 24 within aeroshell 11 is insulated from the tank/thrust structure (FIG. 2). An internal support ring 26 within cavity 24 serves as attachment for lugs 30 on tank/thrust structure 13 via double hinges 50 (FIGS. 3 and 4). The aft end of tank/thrust structure 13 is provided with rocket engines and exit nozzles 33, 34, 35 with trunnion support 37 supporting the tank/thrust structure within aeroshell 11.
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申请公布号 |
US4557444(A) |
申请公布日期 |
1985.12.10 |
申请号 |
US19840569371 |
申请日期 |
1984.01.09 |
申请人 |
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION |
发明人 |
JACKSON, L. ROBERT;TAYLOR, ALLAN H. |
分类号 |
B64G1/14;B64G1/40;B64G1/58;(IPC1-7):B64G1/40 |
主分类号 |
B64G1/14 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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