SAE AMS3832C
Roving, Type "S-2" Glass, Epoxy Resin Impregnated.
Standard:
AKA:
- AMS3832
- Revision: C
- 1994-05-01
- Ams P17 Composite Materials Committee
This specification covers continuous, multiple-strand, glass roving of Type "S-2" glass impregnated with a heat-curable epoxy resin matrix and processed to a "B" stage condition.
This roving has been used typically for filament winding of rocket motor cases, pressure vessels, aircraft, and related structures, but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS3832C | 1994-05-01 | Latest | |
| AMS3832B | 1989-10-01 | Historical | |
| AMS3832A | 1979-07-01 | Historical | |
| AMS3832 | 1970-11-01 | Historical |
- SAE AMS 3832
- Aerospace
- Composite materials
- Fabrics
- Fibers
- Glass
- Lightweight materials
- Plastics
- Resins
- Materials properties