BEHAVIOR OF HYDROXYL-TERMINATED POLYETHER (HTPE) COMPOSITE ROCKET PROPELLANTS IN SLOW COOK-OFF

International Journal of Energetic Materials and Chemical Propulsion ◽

10.1615/intjenergeticmaterialschemprop.v7.i3.10 ◽

2008 ◽

Vol 7 (3) ◽

pp. 171-185 ◽

Author(s):

Rodrigo I. Caro ◽

John M. Bellerby

Keyword(s):

Rocket Propellants

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HIGH BURNING RATE SOLID ROCKET PROPELLANTS

International Journal of Energetic Materials and Chemical Propulsion ◽

10.1615/intjenergeticmaterialschemprop.v4.i1-6.610 ◽

1997 ◽

Vol 4 (1-6) ◽

pp. 646-660 ◽

Author(s):

G. Doriath

Keyword(s):

Burning Rate ◽

Rocket Propellants ◽

Solid Rocket ◽

Solid Rocket Propellants

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Application of high density-impulse nuclear- rocket propellants in aerobraking spacecraft assemblies

10.2514/6.1968-574 ◽

1968 ◽

Author(s):

W. DOWDY

Keyword(s):

High Density ◽

Rocket Propellants ◽

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Explosives for civil uses. Propellants and rocket propellants

10.3403/02956063 ◽

2003 ◽

Keyword(s):

Rocket Propellants

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Explosives for civil uses. Propellants and rocket propellants

10.3403/02856654u ◽

2015 ◽

Keyword(s):

Rocket Propellants

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Explosives for civil uses. Propellants and rocket propellants

10.3403/03145094u ◽

2015 ◽

Keyword(s):

Rocket Propellants

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Estimate of Chemical Space Heating Rates in Gas-Phase Combustion With Application to Rocket Propellants

ARS Journal ◽

10.2514/8.5026 ◽

1960 ◽

Vol 30 (2) ◽

pp. 179-185 ◽

Author(s):

DAVID A. BITTKER ◽

RICHARD S. BROKAW

Keyword(s):

Gas Phase ◽

Chemical Space ◽

Space Heating ◽

Heating Rates ◽

Rocket Propellants

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Nitroglycerine (NG) Migration to Various Unsaturated Polyesters and Chloropolyesters Used for Inhibition of Rocket Propellants

Propellants Explosives Pyrotechnics ◽

10.1002/(sici)1521-4087(199912)24:6<371::aid-prep371>3.0.co;2-l ◽

1999 ◽

Vol 24 (6) ◽

pp. 371-378 ◽

Author(s):

J. P. Agrawal ◽

N. T. Agawane ◽

R. P. Diwakar ◽

R. Chandra

Keyword(s):

Unsaturated Polyesters ◽

Rocket Propellants

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Stabilizer Reaction is Cast Double Base Rocket Propellants. Part VIII: Characterization of propellant gassing properties during simulated aging

Propellants Explosives Pyrotechnics ◽

10.1002/prep.19960210512 ◽

1996 ◽

Vol 21 (5) ◽

pp. 276-283 ◽

Author(s):

M. H. Sammour

Keyword(s):

Rocket Propellants ◽

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Studies on azotetrazolate based high nitrogen content high energy material spotential additives for rocket propellants

Journal of Thermal Analysis and Calorimetry ◽

10.1007/s10973-004-0446-z ◽

2004 ◽

Vol 78 (3) ◽

pp. 781-792

Author(s):

R. Sivabalan ◽

M. B. Talawar ◽

N. Senthilkumar ◽

B. Kavitha ◽

S. N. Asthana

Keyword(s):

Nitrogen Content ◽

High Energy ◽

High Nitrogen Content ◽

High Nitrogen ◽

Rocket Propellants ◽

Energy Material ◽

High Energy Material

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Nano-aluminum as energetic material for rocket propellants

Materials Science and Engineering C ◽

10.1016/j.msec.2006.09.030 ◽

2007 ◽

Vol 27 (5-8) ◽

pp. 1393-1396 ◽

Author(s):

L. Meda ◽

G. Marra ◽

L. Galfetti ◽

F. Severini ◽

L. De Luca

Keyword(s):

Energetic Material ◽

Rocket Propellants

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