METHOD OF RE-ENTRY BODY SEPARATION AND EJECTION
Assignee
Filed
Jun 30, 1977
Granted
Oct 11, 1983
Location
Abstract
A method of separating and ejecting a re-entry body from a booster rocket thout tip-off by igniting a pair of diametrically opposed rockets attached to the base of the re-entry body which provide thrust at an angle, and then firing a plurality of pyrotechnically operated separation nut assemblies, with the attachment bolts being captured in bolt catcher assemblies, to separate the re-entry body from the booster rocket, the pair of rockets providing separation velocity and spin to the re-entry body.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Mar 3, 1982
Rescinded
Mar 2, 1983
Duration
12 months
Record Details
- Patent number
- US 4408536
- Application
- 05819447
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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