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Binders form the mechanical linkage in the rocket fuel. Some binders are also used as fuels. These binders are known as "energetic binders" and are normally hazardous.

R-45M 45 M - A type of Hydroxyl Terminated Polybutadiene commonly used as a binder(HTPB) . Contains a pre-mixed anti-oxidant for long term storage

R-45 HTLO -  A type of HTPB that contains no anti-oxidants. Lower viscosity than R-45M

Low Molecular Weight HTPB - Very low viscosity HTPB. Lower molecular weight. May improve castability and performance. May detrimentally affect density.

Polybutadiene Acrylonitrile (PBAN) - Common hobby binder. Requires Cure schedule. Also used in the Space Transportation System's Solid Rocket Boosters.

Polydimethylsiloxane (PDMS) - 

Curative

These chemicals begin the polymerization of the binder

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These chemicals reduce the viscosity of the uncured propellant. They make mixing and casting of propellants easier and facilitate higher solids loading.

Isodecyl PelargonatePelargonate 

Dioctyl Adipate (DOA)

Dioctyl Sebacate

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Prussian Blue - Blue Powder. Produces a blue tinted propellant after curing.

Methylene Blue - Blue stain. Liquid. Helps lower solid loading.

Nigrosin - Very blackBest opacifier by mass.

TiO2 - Opacifier. Rejects radiative heating. Creates white propellant.

Fuels

Aluminum - More energetic than magnesium but requires a larger motor to properly take advantage of. Large incompletely burned particle can damage nozzle. Tendency to deposit slag inside motor.

Magnesium - Powdered. Burns completely, faster than aluminum. Useful in smaller motors.

Oxidizers

Substances which oxidize the fuel and binder to facilitate combustion.

Ammonium Perchlorate - Most common in amateur and professional composite propellants

Ammonium Nitrate - Extremely hygroscopic. Tends to produce a slower burning propellant than ammonium perchlorate.

Potassium Nitrate - Used commonly in "rocket candy" formulations. Lower performance than ammonium perchlorate or ammonium nitrate.

Stabilizers

Magnesium Oxide

Phenylnaphthalene

DTBHQ - 2,5-ditert-butylhydroquinone

Processing Aids

Lecithin

Silicon Oil - Reduces adherence to mixing bowl. Makes propellant pour better.

Polydimethylsiloxane (PDMS) - Surfactant, reduces sticking to the bowl and aeration during mixing. Allows for mixing at higher speeds. Improves particle wetting.

Binding Agents

Binding agents form a bond between the surface of Ammonium Perchlorate particles and the polymer matrix, embedding the particles strongly in the propellant web. This slightly slows burn rate and increases hardness.

HX-752 - Does not cause foaming. Requires refrigeration. Smells bad.

HX-878 (Tepanol) - May cause foaming due to ammonia generation during curing.

HX-868 - (Dynamar) Co-active with HX-752, increases functionality and decreases migration

Cross Linking Agents

Castor Oil - provides additional sites for the polymer chains to cross link with the curative and castor oil. Increases cured propellant hardness.

Chromatic Burn Additives

Copper Oxychloride - Blue (5%-10% by mass)

Strontium Carbonate - Red.

Flame Retardants

Melamine - Used when using HTPB as a liner material

Zinc Borate - improves char layer formation