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

M. H. Sammour

doi:10.1002/prep.19960210512

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 ◽

Cited By ~ 1

Author(s):

M. H. Sammour

Keyword(s):

Rocket Propellants ◽

Double Base

Characterization of Some Modified Unsaturated Polyesters for Inhibition of Double-base Rocket Propellants

International Journal of Polymer Analysis and Characterization ◽

10.1080/10236660108033958 ◽

2001 ◽

Vol 6 (5) ◽

pp. 415-436

Author(s):

J. P. Agrawal ◽

R. R. Samudra ◽

N. T. Agawane

Keyword(s):

Unsaturated Polyesters ◽

Rocket Propellants ◽

Double Base

Comparative study of unsaturated halo and nonhalo polyesters and inhibition of double-base rocket propellants

Journal of Applied Polymer Science ◽

10.1002/app.1993.070500920 ◽

1993 ◽

Vol 50 (9) ◽

pp. 1655-1664 ◽

Cited By ~ 9

Author(s):

J. P. Agrawal ◽

K. S. Kulkarni

Keyword(s):

Comparative Study ◽

Rocket Propellants ◽

Double Base

Characterization of New Lead-free Ballistic Modifiers and Phthalate-free Plasticizers in Propellants

Journal of Aerospace Technology and Management ◽

10.5028/jatm.etmq.54 ◽

2020 ◽

pp. 15-18

Author(s):

Rosane Macchiarulo Jorge ◽

Acácio Antonio Mesquita Furtado Filho

Keyword(s):

Chemical Compound ◽

Lead Free ◽

Synthesis And Characterization ◽

Ballistic Performance ◽

Ballistic Modifiers ◽

Reduced Toxicity ◽

Double Base ◽

Copper Salicylate

This paper describes the synthesis and characterization of a copper-based ballistic modifier, copper subsalicylate (monobasic copper salicylate), and its performance in green-type propellants. New lead-free ballistic modifiers and phthalatefree plasticizers with reduced toxicity, less harmful to the environment, have been employed to replace their traditional additives in green-type double-base propellant preparations. The characterization of the chemical compound was performed by FTIR, TGA-DSC, and WAXS, indicating that copper subsalicylate was obtained. The results of the characterization of propellant compositions showed that copper subsalicylate, in combination with a bismuth salt, could be a substitute for the traditional lead-based ballistic modifier producing green-type propellants without reducing ballistic performance.

Physical aging of double-base rocket propellants

10.2514/6.1980-1168 ◽

1980 ◽

Cited By ~ 1

Author(s):

P. GREIDANUS ◽

L. STRUIK

Keyword(s):

Physical Aging ◽

Rocket Propellants ◽

Double Base

Tetrachloro Phthalic Anhydride Based Chloropolyesters for Inhibition of Double Base Rocket Propellants

Defence Science Journal ◽

10.14429/dsj.36.5989 ◽

1986 ◽

Vol 36 (4) ◽

pp. 409-420 ◽

Cited By ~ 4

Author(s):

J. P. Agrawal ◽

K. S. Kulkarni

Keyword(s):

Phthalic Anhydride ◽

Rocket Propellants ◽

Double Base

Polysiloxane-based inhibition system for double-base rocket propellants

Journal of Applied Polymer Science ◽

10.1002/(sici)1097-4628(19980705)69:1<7::aid-app2>3.0.co;2-n ◽

1998 ◽

Vol 69 (1) ◽

pp. 7-12 ◽

Cited By ~ 4

Author(s):

J. P. Agrawal ◽

S. Venugopalan ◽

Javed Athar ◽

J. V. Sabane ◽

M. Muralidharan

Keyword(s):

Rocket Propellants ◽

Double Base

Stabilizer reactions in cast double base rocket propellants. Part I: HPLC Determination of Stabilizers and their derivatives in a propellant containing the stabilizer mixture para-nitro-N-methylaniline and 2-nitrodiphenylamine aged at 80°C and 90°C

Propellants Explosives Pyrotechnics ◽

10.1002/prep.19910160507 ◽

1991 ◽

Vol 16 (5) ◽

pp. 235-239 ◽

Cited By ~ 18

Author(s):

J. M. Bellerby ◽

M. H. Sammour

Keyword(s):

Hplc Determination ◽

Rocket Propellants ◽

Double Base

Effect of Certain Barium and Cobalt Salts on the Burning Rate- Pressure Relationship of Double Base Rocket Propellants

Combustion Science and Technology ◽

10.1080/00102208608923851 ◽

1986 ◽

Vol 45 (3-4) ◽

pp. 213-219 ◽

Cited By ~ 1

Author(s):

K. V. Raman ◽

Haridwar Singh ◽

K. R. K. Rao

Keyword(s):

Burning Rate ◽

Rocket Propellants ◽

Double Base ◽

Relationship Of

Technology of the Screw-Extrusion Process for the manufacture of double-base rocket propellants

Propellants Explosives Pyrotechnics ◽

10.1002/prep.19770020402 ◽

1977 ◽

Vol 2 (4) ◽

pp. 69-74 ◽

Cited By ~ 2

Author(s):

A. Homburg ◽

H. Brachert

Keyword(s):

Extrusion Process ◽

Rocket Propellants ◽

Screw Extrusion ◽

Double Base

Development trends in artillery ammunition propellants

Materiały Wysokoenergetyczne / High Energy Materials ◽

10.22211/matwys/0196 ◽

2020 ◽

pp. 5-16

Author(s):

Mateusz Szala

Keyword(s):

Foreseeable Future ◽

Short History ◽

Single Base ◽

Rocket Propellants ◽

Advantages And Disadvantages ◽

Synthetic Rubber ◽

Different Types ◽

History Of ◽

Double Base

A short history of nitrocellulose (NC) use in propellants is discussed. The advantages and disadvantages of NC as a semi-synthetic component of powders and rocket propellants are presented. Based on the conventional classification of propellants, the options of eliminating nitrocellulose in different types of powders and rocket propellants are discussed in detail. The analysis shows that in the foreseeable future, the elimination of NC in single-base and double-base propellants is highly unlikely. The observed trends in triple-base propellant development also does not show any tendencies in the elimination of NC, only the replacement of nitroguanidine with cyclic nitroamines. However, the elimination of NC in LOVA composite propellants is probable. Synthetic, rubber-based solid composite rocket propellants, with ammonium perchlorate as the oxidizer, are the only ones not dependent on NC.