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    • 96. 发明公开
    • Multiple space vehicle launch system
    • Startsystemfürmehrere Raumfahrzeuge
    • EP2662287A1
    • 2013-11-13
    • EP13167339.4
    • 2013-05-10
    • The Boeing Company
    • Aston, Richard WTomzynska, Anna MCaplin, Glenn N
    • B64G1/00B64G1/64
    • B64G1/641B64G1/002B64G1/40B64G1/405B64G1/645
    • A multiple space vehicle launch system (10) that may be adapted to be disposed within a payload region (20) of a launch vehicle fairing (14). The launch system may include a first space vehicle (16), a second space vehicle (18) releasably attached to the first space vehicle (16) and oriented relative to the first space vehicle (16) such that, when placed within the fairing (14), a launch load of the first space vehicle (16) is transmitted to and borne by the second space vehicle (18). In certain embodiments, the first and second space vehicles (16, 18) each may include one of an electrical propulsion unit (40) and a hybrid chemical and electrical propulsion unit (42). Use of electrical or hybrid chemical and electrical propulsion units (40, 42) enables the second space vehicle (18) to bear all or a significant portion of the launch load of the first space vehicle (16), thereby eliminating the need for additional support structure.
    • 多空间车辆发射系统(10),其可以适于被布置在运载火车整流罩(14)的有效载荷区域(20)内。 发射系统可以包括第一空间飞行器(16),可释放地附接到第一空间飞行器(16)并相对于第一空间飞行器(16)定向的第二空间飞行器(18),使得当放置在整流罩 如图14所示,第一空间飞行器(16)的发射载荷被第二空间飞行器(18)传送并承载。 在某些实施例中,第一和第二太空车辆(16,18)各自可以包括电推进单元(40)和混合化学和电力推进单元(42)中的一个。 电气或混合化学和电力推进装置(40,42)的使用使得第二太空车辆(18)承受第一空间飞行器(16)的发射载荷的全部或大部分,从而不需要额外的支撑 结构体。