HIGH STRAIN CAPABILITY BALLISTIC TEST DEVICE FOR SOLID PROPELLANT ROCKET MOTORS
Assignee
MORTON THIOKOL INC.
Filed
Apr 18, 1986
Granted
Jul 26, 1988
Location
Huntsville AL (NASA/Army)
Abstract
A ballistic test device for simulating propellant and/or bond and/or strain conditions in a high pressure, high strain rate rocket motor. The device uses internal compliant sleeves which allow radial expansion or growth of propellants, liners and insulation or any combination of all three.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Jul 30, 1986
Rescinded
Jun 30, 1987
Duration
11 months
Inventor
- 1REXFORD D. ATCHLEY
Sensitive facility: Huntsville AL (NASA/Army)
Record Details
- Patent number
- US 4759215
- Application
- 06853588
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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