| 摘要 |
PROBLEM TO BE SOLVED: To provide a partition structure for a rocket fairing capable of obtaining a wide envelope range for a satellite close to a propulsion rocket main body. SOLUTION: At a tip part 35 of a propulsion rocket main body 31, a fairing 30 for forming plural containing spaces 36, 37 for containing satellites 32, 33 is provided, the satellites 32, 33 are supported on the side of the propulsion rocket main body 31 in the containing spaces 36, 37 by support bases 51, 54, and in parting the satellites 32, 33 from the support bases 51, 54, circumferential walls 43, 44 enclosing the support bases 51, 54 are split to open the containing spaces 36, 37 in this partition structure for a propulsion rocket fairing, where the circumferential walls 43, 44 to enclose the satellite 32 disposed to be closer to the propulsion rocket main body 31 are split to circumferential wall parts 52, 53 to be head-opened in such directions as to get apart from the satellite 32.
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