Invention Grant
US5399599A Thermoplastic elastomeric internal insulation for rocket motors for low
temperature applications
失效
用于低温应用的火箭发动机的热塑性弹性体内部绝缘
- Patent Title: Thermoplastic elastomeric internal insulation for rocket motors for low temperature applications
- Patent Title (中): 用于低温应用的火箭发动机的热塑性弹性体内部绝缘
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Application No.: US39044Application Date: 1993-04-06
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Publication No.: US5399599APublication Date: 1995-03-21
- Inventor: David G. Guillot
- Applicant: David G. Guillot
- Applicant Address: UT Ogden
- Assignee: Thiokol Corporation
- Current Assignee: Thiokol Corporation
- Current Assignee Address: UT Ogden
- Main IPC: C08K13/02
- IPC: C08K13/02 ; C08J3/20 ; C08K5/49 ; C08L77/00
Abstract:
Thermoplastic elastomeric ablative insulation having good mechanical properties at extremely low temperatures are disclosed. The insulation is based upon a polyamide-ether resin and includes carefully selected fillers to possess good low temperature mechanical properties and still provide suitable charring and ablative insulation performance at low temperatures (-65.degree. F.). A typical insulation within the scope of the present invention includes a polyamide-ether thermoplastic elastomeric polymer resin, an inorganic phosphorus containing compound, such as ammonium polyphosphate, present in the insulation from about 5 to about 60 phr, and a polyhydric alcohol present, such as pentaerythritol, in the insulation from about 1 to about 30 phr. The insulation compositions within the scope of the present invention optionally include silicone resin present in the insulation in range from about 0 to 15 phr. Chopped fiber filler may also be present in the insulation in range from about 0 to 100 phr.
Public/Granted literature
- USD375454S Bottle Public/Granted day:1996-11-12
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