| 摘要 |
A spacecraft structure comprises a hollow inner cylindrical member and a plurality of planar bulkheads secured to the outer surface of the inner member and extending radially outwardly from the inner member. A plurality of planar enclosure panels are secured to the extended edges of the bulkheads and each other to form an enclosed spacecraft structure. Suitable payload equipment is secured to the enclosure panels while an apogee kick motor is secured within the inner member.
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