Propellant solid

T. L. Boggs in K. K. Kus and M. Summerfield, eds.. Fundamentals of Solid-Propellant Combustion, Progress in Pistronautics andPieronautics, Vol. 90, AIAA,... [Pg.28]

A. E. Oberth, Principles of Solid Propellant Development, CPIA, Pubhcation 469, Chemical Propulsion Information Agency (CPIA), Johns Hopkins University, Laurel, Md., Sept. 1987. [Pg.53]

Solid Propellant Selection and Characterisation, Space Vehicle Design Criteria, Monograph no. SP 8064, NASA, Airport, Md., 1971. [Pg.53]

G. R. Nickerson and co-workers, M Computer Program for the Prediction of Solid Propellant Motor Peformance, Vols. 1, 2, and 3, AREPL-TR-80-34, AFRPL, Dayton, Ohio, Apr. 1981. [Pg.53]

R. Stenson, Tactors Governing the Storage Tfe of Solid Propellant Pocket Motors, report no. TN047, Explosive Research and Development Establishment, Waltham Abbey, UK, 1972. [Pg.54]

G. K. Adams, in Proceedings of the Fourth Symposium of Naval Structural Mechanics Mechanics and Chemisty of Solid Propellants, Pergamon Press, Inc., New York, 1967, p. 117. [Pg.54]

M. Summerfield and co-workers, in M. Summerfield, ed.. Solid Propellant Research, Aca demic Press, Inc., New York, 1960. [Pg.54]

M. W. Beckstead and K. P. B>x.ooks,A.Modelfor Distributed Combustion in Solid Propellants, Vol 2, CPIA Pubhcation 557, CPIA, Johns Hopkins University, Laurel, Md., Nov. 1990, p. 227. [Pg.54]

R. R. Miller and co-workers. Ballistic Control of Solid Propellants, Hercules, Inc., Rpt. AFRPL-81-058, Dayton, Ohio, 1981. [Pg.54]

P. Kuent2mann, Specific Impulse Tosses ofMetalli d Solid Propellants, PTD-NC-23-2717-74, Air Eorce Eoreign Technology Division, Wright Patterson Air Eorce Base, Dayton, Ohio, 1974. [Pg.55]

T. L. Boggs and R. L. Derr, eds., Ha ard Studiesfor Solid Propellant Pocket Motors, NATO Advisory Group for Aerospace Research and Development, Agardograph 316, Technical Press, London, Sept. 1990. [Pg.55]

Solid Propellant Manuals, issued by the Army Material Command, AMC 706—175, 1961, and AMC 706—176, 1961. [Pg.57]

CPIA.I M2 Solid Propellant Manual, CPIA, Johns Hopkins University, Laurel, Md., 1969. [Pg.57]

F. X. Hartman, Solid Propellants Safety Handbook, Spriagfield, Va., 1965. [Pg.57]

C. Huggett, C. E. Bardey, and M. M. Mills, Solid Propellant Pockets, Princeton University Press, N.J., 1960. [Pg.57]

Monographs on rockets and rocket propellants by the National Aeronautics and Space Administration (NASA), Lewis Research Center, Cleveland. These iaclude the foUowiag Solid Propellant Selection and Characteri tion, Report SP-8064,1971 Solid Rocket Motor Peformance, Report SP-8039,1971 Solid Rocket Motor Igniters, Report SP-8051,1971 Solid Rocket Motor Metal Cases, Report SP-8025, 1970, and Captive Eire Testing of Solid Rocket Motors, Report SP-8041,1971. [Pg.57]

As an energetic polymer, poly(glycidyl azide) (PGA) mance solid propellant binder [63,64]. For this purpose,... [Pg.733]

A solid propellant is a mechanical (heterogeneous) or a chemical (homogeneous, or colloidal) mixture of solid-state fuel and oxidizer-rich chemicals. Specially-formed charges of solid propellant (grains) arc placed in the combustion chamber of the solid rocket motor (SRM) at a production facility. Once assembled, the engine does not require additional maintenance, making it simple, reliable and easy to use. [Pg.1019]

Modern composite solid propellant is a mechanical mixture of the powder-like chemicals and a binding resin. The propellant used for the Space Shuttle solid rocket boosters (SRBs) is a typical example of such mixture ... [Pg.1020]

Used tor modern solid propellant engines in military missiles, space launch vehicles and spacecraft. Pollutes environment by toxic exhaust. [Pg.1022]

Rocket engines arc also used for maneuvers in space. Some operations, such as a onetime transfer of a satellite from lower to higher orbit, could be performed by a solid-propellant engine. Yet many complex maneuvers, such as rendezvous and docking with another spacecraft, require multiple engine firings and variable power impulses. Hence modern spacecraft are equipped with an assortment of attitude control engines that usually use liquid storable propellant. [Pg.1072]

Elastomeric Polybutadiene-acrylonitrile Solid propellant binder... [Pg.119]

A form of cooling, and the one of prime interest, concerns ablative cooling. It is essentially a heat and mass transfer process in which mass is expended to achieve thermal dissipation, absorption, and blocking. The process is passive in nature, serves to control the surface temperature, and greatly restricts the flow of heat into the material substrate. As a result of these desirable attributes, ablative cooling (includes use of plastic compositions) has been widely used for thermal protection of solid propellant motors and less extensively in liquid propellant motors. [Pg.123]

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