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DEVICE FOR OVERCOMING THE PROBLEM OF CREW SAFETY DURING A SPACECRAFT LAUNCH AND INPROVE THE JOINTS CONNECTING THE SEGMENTS OF THE SOLID ROCKET BOOSTER
DEVICE FOR OVERCOMING THE PROBLEM OF CREW SAFETY DURING A SPACECRAFT LAUNCH AND INPROVE THE JOINTS CONNECTING THE SEGMENTS OF THE SOLID ROCKET BOOSTER
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机译:克服航天飞机发射过程中机组安全问题并改善连接固体火箭助推器段的接头的装置
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摘要
Spacecraft, satellites, aircraft and powder rocket launchers are provided with similar clamping devices comprising a housing (6-41), a sleeve (9-42) and the clamping screw (11-15). The housing (6) consists of a stop ring (7) and the sleeve (9) of a number of sectors (10) provided with a modular multiple thread. The clamping screw (11-15) are formed of a towing hook engageable with a stop ring (7) and are provided with a similar modular thread so that the sectors (10) are screwed into the clamping screw (11-15) so as to attach the detachable sections. In addition, spacecraft, satellites and planes are provided with an actuator mechanism which disconnects the joined sections. Explosive charges may be fired by means of a gear mounted ejection and disposed on an interrupt line between sections and can separate the sections from the rest. The parachutes (4), which are in the parachute bag, are released one at a time or in a predetermined order and the crew capsule (2) or the compartment in which persons are supported in on board allows a soft landing and sure.
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