Patent
Ignition system for igniting a gas generator by the use of combustion gases from a solid propellant rocket motor having selective zoning capabilities
Glenn E Webb
- 01 Apr 1969
15
TL;DR: In this article, the authors present an experiment with an opposition system between the COMBUSTION CHAMBER of a GAS GENERATOR and a SRS MOTOR.
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Abstract: AN IGNITION SYSTEM POSITIONED BETWEEN THE COMBUSTION CHAMBER OF A GAS GENERATOR HAVING A SOLID PROPELLANT GRAIN THEREIN AND THE COMBUSTION CHAMBER OF A SOLID PROPELLANT ROCKET MOTOR HAVING SELECTIVE ZONING CAPABILITIES SO THAT WHEN THE IGNITION SYSTEM IS OPERATED THE COMBUSTION GASES FROM THE COMBUSTION CHAMBER OF THE SOLID PROPELLANT ROCKET MOTOR WILL ENTER THE COMBUSTION CHAMBER IN THE GAS GENERATOR AND IGNITE THE SOLID PROPELLANT GRAIN THEREIN.
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Citations
Patent
Solid propellant canister loaded multiple pulsed or staged rocket
Bradley W. Smith,Dean C. Youngkeit +1 more
- 20 Mar 1990
TL;DR: In this paper, a multi-pulse or multi-stage canister loaded solid propellant rocket motor is installed in a monolithic case which affords stiffness continuity over the length of the rocket motor to prevent guidance system upsetting free play.
27
Patent
Multi-burn solid fuel restartable rocket and method of use
Thomas W. Bastian,J. Sydney Roberts +1 more
- 14 Apr 1980
TL;DR: A multi-burn restartable solid rocket fuel having plural layers, each independently ignitable, including a central core, and at least one outer cylindrical layer separated from the central core by a non-ignitable layer is defined in this article.
25
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Hydrostatic control device, particularly steering device
Hans Christian Petersen,Erik Kyster,Svend Erik Thomsen +2 more
- 21 Nov 1983
TL;DR: In this paper, a steering control system for a bidirectional servomotor connectable to steerable wheels is described, in which a rod extending from one side of a piston thereof causes the effective areas on opposite sides of the piston to be unequal.
19
Patent
Reverse bulged forward acting scored rupture disc bulkhead structure for multi-stage rocket motor
Donald Hibler,James Hinrichs +1 more
- 10 Aug 1989
TL;DR: In this article, a burst disc bulkhead is constructed for the use in a multi-stage rocket motor for missiles or the like, where the disc is supported by a multiple apertured backup member and a series of bulges define dimples that conform to the configuration of the apertures.
19
Patent
Missile launching and orientation system
Ivan Ivanovitch Arkhangelsky,Eugene Gueorguevitch Bolotov,Vladimir Sergueevitch Philippov,Vladimir Yakovlevitch Mizrokhi,Vladimir Grigorievitch Svetlov,Gregory Andreevitch Stanevsky,Serge Grigorievitch Khitenkov,Victor Leonidovitch Gaidoukevitch,Eugène Afanassievitch Chmikov +8 more
- 27 Oct 1995
TL;DR: In this article, the authors present an approach to modernize a missile with an inclined launch at an angle by transforming them into missiles controlled for circular defense, avoiding ejection of the passive mass within the launching area.
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