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Study of Aging Characteristics for Metalized HTPB Based Composite Solid Propellants Stored in Ambient Conditions
by
Jain, Prakhar
, Biswas, Shelly
, Rathi, Vineet Kumar
in
Aging
/ Aging (metallurgy)
/ Aluminum
/ Ammonium perchlorates
/ Atmospheric moisture
/ Bimetals
/ Chemical composition
/ Composite propellants
/ Fourier transforms
/ HTPB propellants
/ Infrared analysis
/ Infrared spectroscopy
/ Metal oxides
/ Military applications
/ Missiles
/ Oxidation
/ Parameters
/ Propellant chemistry
/ Propellant decomposition
/ Rocket propellants
/ Rockets
/ Service life
/ Solid propellant rocket engines
/ Solid propellants
/ Solid rocket propellants
/ Thermogravimetric analysis
/ X-ray diffraction
2024
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Study of Aging Characteristics for Metalized HTPB Based Composite Solid Propellants Stored in Ambient Conditions
by
Jain, Prakhar
, Biswas, Shelly
, Rathi, Vineet Kumar
in
Aging
/ Aging (metallurgy)
/ Aluminum
/ Ammonium perchlorates
/ Atmospheric moisture
/ Bimetals
/ Chemical composition
/ Composite propellants
/ Fourier transforms
/ HTPB propellants
/ Infrared analysis
/ Infrared spectroscopy
/ Metal oxides
/ Military applications
/ Missiles
/ Oxidation
/ Parameters
/ Propellant chemistry
/ Propellant decomposition
/ Rocket propellants
/ Rockets
/ Service life
/ Solid propellant rocket engines
/ Solid propellants
/ Solid rocket propellants
/ Thermogravimetric analysis
/ X-ray diffraction
2024
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Do you wish to request the book?
Study of Aging Characteristics for Metalized HTPB Based Composite Solid Propellants Stored in Ambient Conditions
by
Jain, Prakhar
, Biswas, Shelly
, Rathi, Vineet Kumar
in
Aging
/ Aging (metallurgy)
/ Aluminum
/ Ammonium perchlorates
/ Atmospheric moisture
/ Bimetals
/ Chemical composition
/ Composite propellants
/ Fourier transforms
/ HTPB propellants
/ Infrared analysis
/ Infrared spectroscopy
/ Metal oxides
/ Military applications
/ Missiles
/ Oxidation
/ Parameters
/ Propellant chemistry
/ Propellant decomposition
/ Rocket propellants
/ Rockets
/ Service life
/ Solid propellant rocket engines
/ Solid propellants
/ Solid rocket propellants
/ Thermogravimetric analysis
/ X-ray diffraction
2024
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Study of Aging Characteristics for Metalized HTPB Based Composite Solid Propellants Stored in Ambient Conditions
Journal Article
Study of Aging Characteristics for Metalized HTPB Based Composite Solid Propellants Stored in Ambient Conditions
2024
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Overview
The aging of any propellant is defined as the change in the physical, chemical, and performance parameters of solid rocket propellants. The propellant’s service life and aging properties are important parameters of the study, especially for missiles and other defense applications. Hydroxyl-terminated polybutadiene (HTPB) based composite solid propellants with ammonium perchlorate (AP) are the most prominently used propellants in the operations of solid rocket motors in the defense and space sectors. Thus, studying this composite solid propellant is of essential when determining ambient service life. Performance parameters studied in this research are burn rate under high-pressure conditions in Crawford bomb setup, Thermogravimetric Analysis, and Fourier Transform Infrared Spectroscopy (FTIR). SEM and X-ray diffraction (XRD) analysis of the aged sample were also conducted to ascertain the chemical composition and morphological changes in the samples. Naturally aged propellant strands manufactured in different years have been compared with freshly prepared ones to establish a trend for deriving conclusions. The results from different analysis techniques, FTIR, XRD, and FESEM, depicted that oxidation of metals happens while aging of propellant due to atmospheric moisture, and the metal oxides prominently affect the propellant chemical composition and decomposition process of the propellant samples. The ballistic properties of the aluminium added samples showed an increment in burn rate. In contrast, the bimetal addition of aluminium and magnesium combined as an additive decreased the ballistic burn rate.
Publisher
Defence Scientific Information & Documentation Centre
Subject
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