Satellite-rocket integrated multifunctional structure aircraft for ground simulation
A ground-simulating and multi-functional technology, which is applied to aircrafts, astronauts, and astronaut guides, etc. It can solve the problems of low payload ratio and poor performance of integrated aircraft, and improve the payload ratio and reduce the structure. Effects of mass and redundant volume
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[0048] (1) Overall layout and envelope size
[0049] The main body of the satellite-rocket integrated multifunctional structure aircraft for ground simulation is a nearly cylindrical shape of Φ1200mm×3211mm (the one including the adapter is Φ1200mm×3283mm). The front end is arranged with the required payload 800, such as high-resolution cameras, communication antennas, etc., which are in the shape of a cylinder of Φ940mm×1203mm; A nearly cylindrical shape of ×1916mm; the rear end of the aircraft with a star-rocket integrated multifunctional structure for ground simulation is connected to the adapter of the carrier, and the envelope size of the adapter is Φ1200mm×500mm.
[0050] A multi-functional solar battery sail panel is installed in each ±Y direction of the star. It is folded on the side of the shared service cabin during the launch phase. Its envelope size is a cylindrical shape of Φ1200mm×1374mm. The array is 1846mm×1374mm, and the distance between the farthest ends of ...
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