Pulsed detonation engines for reaction control systems

Details Pulsed detonation engines for reaction control systems Pulsed detonation engines for reaction control systems

2006-09-15

2008-08-12

Collins, Timothy D. (Department: 3643)

Aeronautics and astronautics

Spacecraft

With propulsion

C244S164000, C060S247000, C060S039380, C060S039760

Reexamination Certificate

active

07410131

ABSTRACT:
Pulsed detonation engines (PDEs) are adapted for use in reaction control systems (RCS), such as thrusters for orbital correction and control (e.g., for earth-orbiting satellites), divert thrust generation and control for space-based interceptor devices, and for missile trajectory correction and motion control. According to one aspect of the invention, PDEs are adapted for motion control of so-called “kill vehicles,” which are small devices, typically launched from satellites, for strategic missile defense.

REFERENCES:
Eidelman, Shmuel; Sharov, Dmitri; and Book, David; “Aerothermodynamics of Pulsed Detonation Engines,” Apr. 6, 2000, Presented at 36th Annual Meeting, Cocoa Beach, FL, 1999, SAIC, pp. 1 to 10.
Eidelman, Shmuel; Sharov, Dmitri; Book, David: Science Applications Inc McLean Va, Equipment and Supplies: Air Breathing (Unconventional), “Aerothermodynamics of Pulsed Detonation Engines,”, http://www.stormingmedia.us/01/0155/A015504.html.
Eidelman, Shmuel, et al, “Pulsed Detonation Engine Experiental and Theoretical Review,” AIAA/SAE/ASME; pp. 857-865; www.fas.org/irp/mystery/pde.htm.
Eidelman, Shmuel; Sharov, Dmitri; Book, David; Apr. 6, 2000; 20020078304 Science Applications, Inc., McLean, VA USA, Scientific and Technical Aerospace Reports, vol. 40, Nov. 1, 2002, p. 20.
DuPont Engineering Polymers Products—Vespel® ; http://www.dupont.com/vespel/.
Claims from co-pending application filed Dec. 9, 2003 (U.S. Appl. No. 10/730,020).
www.aardvark.co.nz/pjet/pde.shtml.
After Combustion: Detonation! By Jim Kelly in Popular Science Aug. 2003.

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