US3992995A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Speed controlled second event launcher
Assignee: United States Department of the Air Force
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Filing: 1975-09-04
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Granted: 1976-11-23
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Expires: 1995-09-04
Abstract
Abstract A variable position launcher including a launch tube in which the second event (SE) package is placed. A positioning spring on the explosive side of the SE package urges it toward the muzzle end of the tube which is sealed with a frangible cover. A gas inlet operates to pressurize the muzzle end of the tube and apply a velocity dependent force on the SE package opposite the spring force so that the SE package is accurately positioned within the tube thereby controlling the retrolaunch velocity.
Inventors
- 👤 Arne H. Wiedermann
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 21:12
CPC Classifications
F; F42; F42B; F42B12/00; F42B12/02; F42B12/36; F42B12/44; F42C; F42C15/00; F42C15/28
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
212 words
A speed controlled variable position launcher system for deploying a high explosive second event package in a detonable fuel-air-explosive (FAE) cloud formed after the bursting of an FAE device, said variable position launcher comprising, an elongated hollow launch tube for attachment to the FAE device, said launch tube having an explosive cavity at one end and a muzzle at the other end, an explosive charge positioned in the explosive cavity of said launch tube, a second event (SE) package slidably positioned in the central portion of said launching tube, a positioning spring disposed in said launch tube between said SE package and the explosive cavity end, said spring operating to urge said SE package toward the muzzle end of said launch tube, a pressure tight frangible cover positioned over the muzzle end of said launch tube, and means for pressurizing the area between said SE package and the muzzle end of said launch tube such that the position of the SE package is dependent on the relationship between the forces exerted by the pressure and by the positioning spring thereby positioning the SE package in a predetermined location in the launch tube to allow launching at the proper velocity and cause the FAE cloud to be detonated when the SE package explodes.
Claim 2
Dependent Claim
212 words
A speed controlled variable position launcher system for deploying a high explosive second event package in a detonable fuel-air-explosive (FAE) cloud formed after the bursting of an FAE device, said variable position launcher comprising, an elongated hollow launch tube for attachment to the FAE device, said launch tube having an explosive cavity at one end and a muzzle at the other end, an explosive charge positioned in the explosive cavity of said launch tube, a second event (SE) package slidably positioned in the central portion of said launching tube, a positioning spring disposed in said launch tube between said SE package and the explosive cavity end, said spring operating to urge said SE package toward the muzzle end of said launch tube, a pressure tight frangible cover positioned over the muzzle end of said launch tube, and means for pressurizing the area between said SE package and the muzzle end of said launch tube such that the position of the SE package is dependent on the relationship between the forces exerted by the pressure and by the positioning spring thereby positioning the SE package in a predetermined location in the launch tube to allow launching at the proper velocity and cause the FAE cloud to be detonated when the SE package explodes.
Claim 3
Dependent Claim
119 words
The speed controlled variable position launcher system defined in claim 1 wherein said second event (SE) package includes, a case having a larger forward section and a smaller rearward section, SE explosive disposed in the larger forward section of said case, a delay unit positioned in the smaller rearward section of said case, a cover disc over the forward section of said case for retaining the SE explosive therein, means for sealing the area between said second event package and the inner wall of said launch tube to prevent pressurized gas leakage between the muzzle area and the explosive cavity end thereby preventing the gas pressure from affecting the biasing pressure on the spring side of the SE package.
Claim 4
Dependent Claim
42 words
The speed controlled variable position launcher system defined in claim 2 wherein a vent is provided in the wall of the launch tube near the explosive cavity end, said vent operating to prevent pressure increase caused by leakage past the sealing means.
Claim 5
Dependent Claim
79 words
The speed controlled variable position launcher system defined in claim 2 wherein said means for pressurizing the area between said SE package and the muzzle end of said launch tube includes a pressure inlet tube in the wall of said launch tube near the muzzle end thereof, said inlet tube being in operative communication with a velocity dependent source of ram air pressure from the FAE device, said pressure varying in proportion to the velocity of the FAE device.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1979-11-23 | 1980-05-24 | 1980-11-23 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1983-11-23 | 1984-05-24 | 1984-11-23 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1987-11-23 | 1988-05-24 | 1988-11-23 | $7700.00 | Window Closed / Lapsed |