Kishore, K and Rajalingam, P (1986) The Bonding Ability and Bonding Site of a New Ferrocene Based Silicon Compound in Composite Solid Propellants. In: Journal of Polymer Science Part C: Polymer Letters, 24 (9). pp. 471-476.
Ammonium perchlorate (AP: 70-85 wt%) and carboxy or hydroxy terminated polybutadiene (CTPB or HTPB: 15-20 wt%) constitute the major ingredients of commonly-used composite solid propellant systems. The polymer, in addition to its function as a fuel, acts as a binder for the structural integrity of the solid propellant.
|Item Type:||Journal Article|
|Additional Information:||The copyright belongs to John Wiley & Sons, Inc.|
|Department/Centre:||Division of Chemical Sciences > Inorganic & Physical Chemistry|
|Date Deposited:||28 Dec 2005|
|Last Modified:||19 Sep 2010 04:22|
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