| Patent Number |
Title Of Patent |
Date Issued |
| 8132492 |
Dispensing device for infrared special material |
March 13, 2012 |
| In accordance with the present invention, there is provided a deployment device that is operative to deploy Special Material (SM) to protect the vehicle when an enemy infrared (IR) threat is present. The deployment device constructed in accordance with the present invention comprises at |
| 7467758 |
Reel-out, reel-in magazine and towline cartridge |
December 23, 2008 |
| Provided is a reel-out reel-in apparatus that is specifically configured to rapidly deploy and retrieve a towed device such as an aerial decoy towed behind an aircraft. The reel-out reel-in apparatus comprises a spool, a towline wound around the spool and connected to the towed devic |
| 6571714 |
Silicon window infrared augmenter |
June 3, 2003 |
| There is provided an electrically powered augmenter device that has a silicon window. The silicon window emits the infrared radiation from the augmenter in a specific waveband, to attract heat seeking missles. Moreover, the augmenter may be mounted on the fuselage of an unpowered aer |
| 6510798 |
Packaging method for infrared special material |
January 28, 2003 |
| A method of packaging a multiplicity of infrared decoy foils into a canister having an aft end and a drive screw extending therein. The present method allows for the controlled dispensing and dispersal of the decoy foils from within the canister and comprises the initial step of asse |
| 6499407 |
Packaging method for infrared special material |
December 31, 2002 |
| A method of packaging a multiplicity of infrared decoy foils into a canister having an aft end and a drive screw extending therein. The present method allows for the controlled dispensing and dispersal of the decoy foils from within the canister and comprises the initial step of asse |
| 6116606 |
High speed glide target |
September 12, 2000 |
| A glide target comprising a fuselage having forward and aft ends. Movably attached to the fuselage is at least one control surface, while releasably attached to the fuselage is a tow line adaptor. Disposed within the fuselage is a tow line adaptor release mechanism which mechanically |
