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公开(公告)号：US3903801A
公开(公告)日：1975-09-09
申请号：US37859573
申请日：1973-07-12
Applicant: SENOSKI WALTER E
Inventor： SENOSKI WALTER E
CPC classification number: F42B8/24
Abstract: A model rocket including novel means for recovering the same after the rocket has spent its fuel and has reached its maximum altitude is provided. The recovery means comprises a foldable rotor assembly which is contained within the rocket body.
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公开(公告)号：US3218997A
公开(公告)日：1965-11-23
申请号：US25677463
申请日：1963-02-06
Applicant: BERGHOUT CHRISTIAN F , MAXWELL DAUER , LANARD FRANCIS W , MINX RAMON P , SENOSKI WALTER E , WARD URAL T
Inventor： BERGHOUT CHRISTIAN F , MAXWELL DAUER , LANARD FRANCIS W , MINX RAMON P , SENOSKI WALTER E , WARD URAL T
IPC: G21F9/32
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公开(公告)号：US3888178A
公开(公告)日：1975-06-10
申请号：US51919274
申请日：1974-10-30
Applicant: SENOSKI WALTER E
Inventor： SENOSKI WALTER E
CPC classification number: F42B8/24
Abstract: A solid fuel-powered model rocket having a main body tube and at least one auxiliary body tube. A solid fuel motor is mounted in the after end of one of the tubes and a slidable plug is disposed in the after end of the other tube, the plug being provided with a latch for engaging a wing elevator and maintaining it parallel to the horizontal plane of the wing against the biasing of a resilient band while the craft is in vertical flight. Following burn-out of the propellant charge, the gases generated upon ignition of a blow-out charge in the fuel cartridge cause rearward displacement of the slidable plug, disengagement of the latch and deployment of the elevator to a predetermined up-angel relative to the top horizontal plane of the wing, thereby directing the craft into a generally horizontal glide attitude.
Abstract translation: 一种固体燃料动力型火箭，其具有主体管和至少一个辅助体管。 固体燃料电动机安装在其中一个管的后端，并且可滑动的塞子设置在另一个管的后端，插头设置有用于接合机翼升降机并保持其平行于水平面的闩锁 的机翼抵抗弹性带的偏压，同时飞行器处于垂直飞行。 在燃料喷射燃料燃烧之后，燃料筒中的吹出电荷点火时产生的气体引起滑动插头向后的位移，闩锁的分离和电梯的展开相对于预定的上升天使 机翼的顶部水平面，从而将飞行物引导到大体上水平的滑翔姿态。
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