Patent EP0451882A2 successfully refreshed from Google Patents.
Patent US4553718A successfully refreshed from Google Patents.
US4553718A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Naval harrassment missile
Assignee: Boeing Co
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Filing: 1982-09-30
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Granted: 1985-11-19
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Expires: 2002-09-30
Abstract
Abstract A naval harrassment missile for autonomously flying to a designated target area such as an enemy naval warship. The missile designed for searching, finding and harrassing the target. The missile may send a homing signal to guide other missiles to the target or by a homing signal attack the target using either a high explosive or a self-forging fragmentation warhead.
Inventors
- 👤 George T. Pinson
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-07 11:45
CPC Classifications
F; F41; F41G; F41G7/00; F41G7/20; F41G7/22; F41G7/226; B; B64; B64U; B64U10/00; B64U10/25; B64U80/00; B64U80/70; B64U80/80; B64U80/84; F41G7/2273; F41G7/2286; F41G7/2293; F42; F42B; F42B10/00; F42B10/02; F42B10/14; F42B12/00; F42B12/02; F42B12/20; F42B12/201; F42B12/204; F42B12/36; F42B12/365; F42B15/00; F42B15/01; F42B15/10; F42B15/105; B64U2101/00; B64U2101/15; B64U2101/18; B64U50/00; B64U50/10; B64U50/13
Claims Analysis
Total Claims: 13
Claim 1
Independent Claim
244 words
A naval harrassment missile for launching frpom shipboard and autonomously flying to a designated target area and attacking a target and providing a homing signal for other missiles to guide them in attacking the target, the missile comprising: a missile airframe with deployed wings, the wings when deployed fixed to the missile for controlling the missile during target harrassment, observation and terminal attack flight; drive means mounted on the airframe for propelling the missile to the target area; a missile flight computer mounted on the airframe and adapted for interfacing with a control computer on shipboard and receiving mission data therefrom, the flight computer receiving a command from the control computer to initiate take-off, the flight computer having preprogrammed information for flight to a designated target area, the flight computer controlling the speed of the drive means; a target sensor mounted on the airframe and activated when the missile arrives in the designated area, the sensor when activated searches for and detects a target, the sensor providing guidance data on the target to the flight computer and control computer, the flight computer and control computer with the target data having the option to instruct the missile to enter a harrassment loiter pattern, an observation pattern and attack the target; and a navigational signal unit mounted on the airframe for providing information to the flight computer and control computer for providing target data to other missiles to guide the other missiles in attacking the target.
Claim 2
Dependent Claim
244 words
A naval harrassment missile for launching frpom shipboard and autonomously flying to a designated target area and attacking a target and providing a homing signal for other missiles to guide them in attacking the target, the missile comprising: a missile airframe with deployed wings, the wings when deployed fixed to the missile for controlling the missile during target harrassment, observation and terminal attack flight; drive means mounted on the airframe for propelling the missile to the target area; a missile flight computer mounted on the airframe and adapted for interfacing with a control computer on shipboard and receiving mission data therefrom, the flight computer receiving a command from the control computer to initiate take-off, the flight computer having preprogrammed information for flight to a designated target area, the flight computer controlling the speed of the drive means; a target sensor mounted on the airframe and activated when the missile arrives in the designated area, the sensor when activated searches for and detects a target, the sensor providing guidance data on the target to the flight computer and control computer, the flight computer and control computer with the target data having the option to instruct the missile to enter a harrassment loiter pattern, an observation pattern and attack the target; and a navigational signal unit mounted on the airframe for providing information to the flight computer and control computer for providing target data to other missiles to guide the other missiles in attacking the target.
Claim 3
Dependent Claim
67 words
The missile as described in claim 1 further including a shipping and storage module for receiving the missile therein, the module including a launch stand for receiving the missile thereon, an automatic starter connected to the drive means for starting the drive means; and an interface connected to the automatic starter for connecting the missile to a launch controller for performing separate tests by a shipboard computer.
Claim 4
Dependent Claim
27 words
The missile as described in claim 1 further including static pressure ports and pitot tube mounted on the airframe for determining static pressure measurements and dynamic pressure.
Claim 5
Dependent Claim
23 words
The missile as described in claim 1 further including gyros mounted on the airframe for providing stabilization data to the missile flight computer.
Claim 6
Dependent Claim
19 words
The missile as described in claim 1 further including a warhead mounted on the airframe for attacking the target.
Claim 7
Dependent Claim
25 words
The missile as described in claim 5 wherein the warhead is a self-forging fragmentation warhead for penetrating the armor plate of an enemy war ship.
Claim 8
Dependent Claim
219 words
A naval harrassment missile for launching from shipboard and autonomously flying to a designated target area and attacking a target and providing a homing signal for other missiles to guide them in attacking the target, the missile comprising: a missile airframe with deployed wings, the wings when deployed controlling the missile during target harrassment, observation and terminal attack flight; an engine drive with propeller for propelling the missile to the target; a missile flight computer mounted on the airframe and adapted for interfacing with a control computer on shipboard and receiving mission data therefrom, the flight computer receiving a command from the control computer to initiate take-off, the flight computer having preprogrammed information for flight to a designated target area, the flight computer controlling the speed of the engine drive; a transmitting and receiving antenna connected to a transceiver for receiving data from the control computer on shipboard or from other missiles; and a target sensor mounted on the airframe and activated when the missile arrives in the designated target area, the sensor when activated searches for and detects a target, the sensor providing target data to the flight computer and control computer, the flight computer and control computer having the option to instruct the missile to enter a harrassment loiter pattern, an observation pattern and attack the target.
Claim 9
Dependent Claim
219 words
A naval harrassment missile for launching from shipboard and autonomously flying to a designated target area and attacking a target and providing a homing signal for other missiles to guide them in attacking the target, the missile comprising: a missile airframe with deployed wings, the wings when deployed controlling the missile during target harrassment, observation and terminal attack flight; an engine drive with propeller for propelling the missile to the target; a missile flight computer mounted on the airframe and adapted for interfacing with a control computer on shipboard and receiving mission data therefrom, the flight computer receiving a command from the control computer to initiate take-off, the flight computer having preprogrammed information for flight to a designated target area, the flight computer controlling the speed of the engine drive; a transmitting and receiving antenna connected to a transceiver for receiving data from the control computer on shipboard or from other missiles; and a target sensor mounted on the airframe and activated when the missile arrives in the designated target area, the sensor when activated searches for and detects a target, the sensor providing target data to the flight computer and control computer, the flight computer and control computer having the option to instruct the missile to enter a harrassment loiter pattern, an observation pattern and attack the target.
Claim 10
Dependent Claim
27 words
The missile as described in claim 7 further including static pressure ports and pitot tube mounted on the airframe for determining static pressure measurements and dynamic pressure.
Claim 11
Dependent Claim
23 words
The missile as described in claim 7 further including gyros mounted on the airframe for providing stabilization data to the missile flight computer.
Claim 12
Dependent Claim
19 words
The missile as described in claim 7 further including a warhead mounted on the airframe for attacking the target.
Claim 13
Dependent Claim
25 words
The missile as described in claim 10 wherein the warhead is a self-forging fragmentation warhead for penetrating the armor plate of an enemy war ship.
References Cited (Backward Citations)
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US4160415A
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US4296894A
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EP0048068A1
Cited
US4471923A
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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) | 1988-11-18 | 1989-05-20 | 1989-11-19 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1992-11-18 | 1993-05-20 | 1993-11-19 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1996-11-18 | 1997-05-20 | 1997-11-19 | $7700.00 | Window Closed / Lapsed |