Combustion Characteristics of AP Based Solid Rocket Propellant

Name: Combustion Characteristics of AP Based Solid Rocket Propellant
Brand: VDM Verlag Dr. Müller
SKU: 9783639371321
Price: 151.33 RON
Availability: InStock

Propellant Selection, Fabrication and Testing

Autor: Amir Aziz, Wan Khairuddin Wan Ali

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Legare: Carte broșată

Editura: VDM Verlag Dr. Müller

Disponibilitate: Disponibil în cantități mici

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151.33 lei

There were many studies on ammonium perchlorate (AP) based solid rocket propellant and some data alr...

Informații despre carte

Autor

Amir Aziz, Wan Khairuddin Wan Ali

Limbă

engleză

Legare

Carte - Carte broșată

Publicat

2011

Pagini

116

EAN

9783639371321

Enbook ID

06843850

Editura

VDM Verlag Dr. Müller

Greutate

174

Dimensiuni

150 x 220 x 6

Descriere completă

There were many studies on ammonium perchlorate (AP) based solid rocket propellant and some data already existed. However, there is no complete data available in Malaysia especially on the information of combustion characteristics of baseline data of AP based SRP. This monograph discusses on the combustion characteristics of AP based SRP including the methods of the propellant selection and fabrication, burning rate test and static thrust test. Thirteen sets of different propellant mixture were prepared with consideration of the mechanical and processability factors. The propellant was a mixture of AP as an oxidizer, aluminum (Al) as fuel and hydroxy-terminated polybutadiene (HTPB) as binder/fuel. By varying the AP and Al, the effect of oxidizer-fuel (O/F) ratio on the whole propellant was determined. The propellant strands were manufactured using press-molding method and burned in a strand burner to obtain the initial burning characteristics. This monograph suitable for those who interested to get better understanding in AP based solid propellant.

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Combustion Characteristics of AP Based Solid Rocket Propellant

Propellant Selection, Fabrication and Testing

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Descriere completă

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