Missile launcher

• US 4,944,210 A
• Filed: 08/08/1988
• Issued: 07/31/1990
• Est. Priority Date: 08/08/1988
• Status: Expired due to Fees

• Current Assignee: Hughes Aircraft Company (Rtx Corporation)
• Original Assignee: Hughes Aircraft Company (Rtx Corporation)
• Inventors: Flock, Thomas G., Baysinger, Scott D.
• Primary Examiner(s): BROWN, DAVID
• Application Number:
  US07/229,882
• Time in Patent Office: 722 Days
• Field of Search: 89/1.818, 89/1.816, 89/1.704, 89/1.705, 89/1.706, 89/1.703, 89/1.7, 89/1.14, 102/530, 102/531
• US Class Current: 89/1.818
• CPC Class Codes: F42B 29/00 Noiseless, smokeless, or flashless missiles launched by their own explosive propellant

Abstract

An elongate gas-tight elastic bag has one open end unitarily secured to an inflator/thruster which can be actuated to rapidly fill the bag with gas. The bag and inflator/thruster are located within a missile launch tube and the bag expands upon being filled with gas to launch the missile.

Claims

1. Apparatus for launching a missile, comprising:

an open-ended tube for receiving the missile therewithin, said tube being longer than the missile and having fore and aft ends;

a selectively actuatable pressurized gas generator having external dimensions enabling sliding receipt of the generator within the tube aft end, said generator having a diffusor through which gas can move along in a first direction and a plurality of openings through which gas can move in a second direction generally opposite to the first direction; and

an expandable, air-tight, bag-like member, said bag-like member having an opening for receiving gas passing through the diffusor,

whereby expansion of said bag-like member causes said missile to be launched from said tube.

2. Apparatus for launching a missile as in claim 1, in which the expandable member is folded onto itself prior to being expanded by gas from the generator.

3. Apparatus for launching a missile as in claim 1, in which the openings are of such a number and dimensions as to produce a gaseous counter thrust to equilibrate the recoil upon missile launch.

4. Apparatus for launching a missile as in claim 1, in which a heat absorbing material is located in the gas generator between the diffusor and the expandable member.

5. Means for launching a missile as in claim 4, in which the heat absorbing member consists of granulated silicon dioxide.

6. Apparatus for launching a missile as in claim 1, in which the expandable member includes an elastic bag having a single opening, said opening adapted to fit onto the gas generator for receiving gas therefrom.

7. Apparatus for launching a missile as in claim 6, in which the elastic bag when expanded is elongate and of such dimensions as to enable sliding receipt within the tube, the combined overall length of the bag and gas generator being substantially the same as the tube length.

8. Apparatus for launching a missile as in claim 6, in which the elastic bag is constructed of nylon fabric and includes a reinforced portion.

9. Apparatus for launching a missile as in claim 8, in which the reinforced portion includes multiple layers of nylon fabric.

10. Apparatus for launching a missile as in claim 6, in which portions of the plastic bag adjacent the opening include a heat insulating material.

11. Apparatus for launching a missile as in claim 10, in which the heat insulating material is a polymeric.