| 摘要 |
FIELD: transport.SUBSTANCE: invention relates to aerospace engineering. Module spacecraft comprises the service system module, the first and second payload modules. The first payload module is arranged at the second one for it to take up the load transferred thereto from the first payload module. Spacecraft comprises the interfaces for power supply, data transfer and other signals and has the sufficient space for accommodation of the larger components: solar battery panels and antennas.EFFECT: decreased weight, accelerated fabrication and ground experimental finishing.3 cl, 4 dwg |
