Optical fiber guided tube-launched projectile system

• US 4,796,833 A
• Filed: 09/08/1987
• Issued: 01/10/1989
• Est. Priority Date: 03/31/1987
• Status: Expired due to Fees

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Pinson, George T.
• Primary Examiner(s): Jordan, Charles T.
• Application Number:
  US07/093,599
• Time in Patent Office: 490 Days
• Field of Search: 244/3.12, 89/1.34, 89/1.8, 89/1.816, 89/1.817
• US Class Current: 244/3.12
• CPC Class Codes: B65H 2701/32 Optical fibres or optical cables
• CPC Class Codes: F41G 7/32 for wire-guided missiles
• CPC Class Codes: F42B 15/04 using wire, e.g. for guiding ground-to-ground rockets

Abstract

In an optical fiber guided projectile system for firing a projectile having trailing and leading ends from a generally tubular launcher and for guiding the projectile to a target wherein the projectile includes an extended length of optical fiber disposed for streaming from the trailing end of the projectile during flight and wherein, prior to firing, a portion of the optical fiber extends from the trailing end of the projectile axially along the inner surface of the tubular launcher and through the mouth of the launcher to a controller, the improvement comprises a generally resilient plug disposed in the launcher between the leading end of the projectile and the mouth of the launcher, the plug securing the portion of the optical fiber in axial orientation along the inner surface of the tubular launcher during firing of the projectile.

Claims

1. In an optical fiber guided projectile system for firing a projectile having trailing and leading ends from a generally tubular launcher and for guiding the projectile to a target, wherein the projectile includes an extended length of optical fiber disposed for streaming from the trailing end of the projectile during flight and wherein, prior to firing, a portion of the optical fiber extends from the trailing end of the projectile axially along the inner surface of the tubular launcher and through the mouth of the launcher to a control means, the improvement comprising:

a generally resilient plug disposed in the launcher between the leading end of the projectile and the mouth of the launcher, said plug securing said portion of the optical fiber in axial orientation along the inner surface of the tubular launcher during firing of said projectile.

2. The system of claim 1 wherein said plug is made of plastic.

3. The system of claim 1 wherein said plug forms an interference fit in said launcher.

4. The system of claim 1 wherein said plug includes a plurality of axial holes for release of gas pressure generated in the launcher during firing.

5. The system of claim 1 including means disposed between said plug and the leading end of said projectile for protecting the leading end of said projectile from damage during launch.

6. The system of claim 1 wherein the end of said plug proximate the leading end of said plug proximate the leading end of said projectile is shaped to receive and to protect the leading end of said projectile during launch.

7. The system of claim 1 wherein said plug comprises a plurality of discs of resilient material for disposition in said launcher in axially spaced relation, each said disc including axial holes for release of gas pressure.