SPACE MODULE Russian patent published in 2017 - IPC B64G1/22 B64G1/40 

FIELD: aviation.

SUBSTANCE: space module (SM) comprises a prismatic power housing of the block type. A one-use (for spacecraft (SC) residual angular velocity bleedoff from SM) gas-rocket launcher is mounted on the front panel. Traction modules with stationary electrojet engines and gas distribution units are mounted on the side panels part which is clear of devices. All panels are designed multi-layer and honeycomb. Eeach traction module is mounted on the carriers which are adjustable relative to the SC with SM mass centre.

EFFECT: fuel weight reduction on the space module board due to the possibility of using rocket engines with a higher specific impulse.

5 dwg