Uses: Mainly used in aerospace solid rocket propellant adhesives. HTPB is cast in engine propulsion system and cured together with oxidizer, aluminum powder and high-energy fuel material for solid rocket and various types of missile propellant binder. In addition, it is also used as a propellant adhesive for propulsion, direction change, escape and deceleration systems of space vehicles.
Packing: 50L closed top polyethylene white plastic drum packaging. Barrel mouth diameter not less than 100mm. Net weight per barrel 50KG.
Specification:
ltems | Hydroxyl-terminated polybutadiene | Test Method | |||||
Type Ⅰ | Type Ⅰ Modified | Type Ⅱ | Type Ⅲ | Type Ⅳ | |||
Hydroxyl value | mmol/g | 0.47-0.53 | 0.54-0.64 | 0.65-0.70 | 0.71-0.80 | Titration | |
Water mass fraction | % | ≤ 0.050 | Karl Fischer Method | ||||
H202 | % | ≤ 0.040 | ≤ 0.050 | Titratian | |||
Viscosity(40°C) | Pa.5 | ≤ 9.5 | ≤ 8.5 | ≤ 4.0 | ≤ 3.5 | Single- drum rotational viscometer method | |
Average molecular weight (x103) | (POV) (GPC) | 3.80-4.60 | 4.00-4.60 | 3.30-4.10 | 3.00-3.60 | 2.70-3.30 | VPO method |
Mass fraction of volatiles | % | ≤ 0.5 | 0.65 | Vacuum drying method | |||
Apperance | Colorless or light yellow transparent liquid, na visually visible impurities | Visual inspection |
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