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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, satellite, aeroplane and solid rocket booster are provided with similar locking device, comprise the housing (6-41), sleeve (9-42) and the screw clamps (11-15). The housing (6) is composite with thrust ring (7) and sleeve (9) with a number of sectors (10), which are provided with a module multiple thread. The screw clamps (11-15) are formed with a draw hook engageable with thrust ring (7) and provided with similar module multiple thread, so that to the sectors (10) screw in the screw with clamps (11-15) to joint the detachable sections. In addition to it, spacecraft, satellite, aeroplane are provided with a tripping mechanism which is disconnecting the joined sections. Explosive charges which may be fired by means of ejection gear mounted and disposed on a break line between sections and carry out detachment the sections from the remainder. The parachutes (4) in the pack are released one at a time or predetermined order and the crew capsule (2) or the compartment with people on board makes a safe, soft landing.
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