IP Library Granted Patent US 8,256,086
Granted Patent B2
US 8,256,086 · App. 12/491,953 · Granted Sep 4, 2012

Method of producing missile nose cones

Assignee: Lockheed Martin Corporation
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 8,256,086
App. No.
12/491,953
Granted
Sep 4, 2012
Kind
B2
Abstract

A method for producing a missile nose cone is disclosed. The method consists of manufacturing a first missile nose cone from a first lot of polymeric material and determining a first rupture value. The method further consists of manufacturing a second missile nose cone from a second lot of polymeric material and determining a second rupture value of the second missile nose cone. Both first and second lots of material are mixed into a test batch with one another based on their associated rupture values. An evaluation missile nose cone is then manufactured from the test batch and a determination is made as to whether the evaluation missile nose cone has a desired rupture value. If a desired rupture value is not obtained, then the mixing and evaluation steps are repeated.

Claims (24)

1. A method for producing a missile nose cone, comprising:

manufacturing a first missile nose cone from a first lot of polymeric material and determining a first rupture value of said first missile nose cone;

manufacturing a second missile nose cone from a second lot of polymeric material and determining a second rupture value of said second missile nose cone;

mixing into a test batch said first and second lots of material with one another based upon said rupture values;

manufacturing an evaluation missile nose cone from said test batch; and

determining whether said evaluation missile nose cone has a desired rupture value.

2. The method according to claim 1 , further comprising:

cutting a hoop section from each said first and second missile nose cones and determining said rupture values from said hoop sections.

3. The method according to claim 2 , further comprising:

positioning said hoop sections into a test fixture which comprises a bladder received within said hoop section, wherein said bladder is expanded until said hoop section ruptures.

4. The method according to claim 1 , further comprising:

designating said lot of polymeric material with a higher comparative rupture value as a dominant resin; and

designating said lot of polymeric material with a lower comparative rupture value as a dilutent resin.

5. The method according to claim 4 , further comprising:

selecting percentage amounts of said dominant and dilutent resins for mixing into said test batch based upon rupture values of each said lot.

6. The method according to claim 5 , further comprising:

cutting a hoop section from said evaluation missile nose cone manufactured from said test batch.

7. The method according to claim 6 , further comprising:

repeating selecting and determining steps until a desired ratio of dominant and dilutent resin obtains said desired rupture value.

8. The method according to claim 7 , further comprising:

fully mixing said first and second lots in said desired ratio; and

manufacturing missile nose cones with said fully mixed lot.

9. The method according to claim 1 , further comprising:

designating said desired rupture value as being between two values.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 25, 2009
From: SHUTLER, ROBERT A.; MANNING, MARGARET ROSE; LEITCH, PAUL A.; LIGGETT, PAUL E.
To: LOCKHEED MARTIN CORPORATION
Reel/Frame 022877/0393 →
Continuity (1)
Related Publication 20100326182A1 · Dec 30, 2010