AERIAL MISSILE HAVING MULTIPLE SUBMISSILES WITH INDIVIDUAL CONTROL OF SUBMISSIBLE EJECTION
Assignee
Boeing
Filed as: BOEING COMPANY, THE
Filed
Oct 6, 1980
Granted
Dec 2, 1986
Location
Huntsville AL (NASA/Army)
Abstract
An aerial missile carrying multiple launching tubes for submissiles in a circular locus about the longitudinal axis of the aerial missile has independent activating means for each said launching tube to pivot the rear discharge end of each launching tube radially outwardly from the aerial missile. Means for ejecting the individual submissile rearwardly from the launching tube are provided. In one embodiment, a single gas generator activates the launching tube and ejects the submissile. Multiple pyrotechnic charges are provided in one embodiment to establish the ejection velocity of the submissile.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Apr 1, 1982
Rescinded
Sep 10, 1985
Duration
3 years, 5 months
Inventor
- 1GEORGE T. PINSON
Sensitive facility: Huntsville AL (NASA/Army)
Record Details
- Patent number
- US 4625646
- Application
- 00619404
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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