Joseph E Pelham DeceasedHuntsville, AL

Joseph Pelham Phones & Addresses

Huntsville, AL

Brigham City, UT

148 N 900 E, Brigham City, UT 84302 (435) 881-4945

Work

Position: Sales Occupations

Education

Degree: Bachelor's degree or higher

Mentions for Joseph E Pelham

Joseph Pelham resumes & CV records

Resumes

Joseph Pelham Photo 25

Joseph Pelham

Location:
United States
Joseph Pelham Photo 26

Joseph Pelham

Location:
United States

Publications & IP owners

Us Patents

Rocket Igniter

US Patent:
3974772, Aug 17, 1976
Filed:
Jun 25, 1958
Appl. No.:
3/745799
Inventors:
Joseph E. Pelham - Huntsville AL
Frank W. La Haye - Hollister CA
Assignee:
Thiokol Corporation - Newtown PA
International Classification:
F42B 508
US Classification:
102 702A
Abstract:
1. An igniter adapted to be positioned in the convergent portion of the nozzle of a rocket engine, said igniter comprising, a tapered combustible plastic casing having a small end and a large end, said casing having a stepped recess therein comprising a large cavity formed in the large end of said casing and a relatively small cavity opening into the inner end of said large cavity, a squib including a primer charge positioned in said small cavity, a body of pyrotechnic material positioned in said large cavity adjacent to said primer charge, a closure disc positioned in said large cavity to hold said pyrotechnic material therein, and squib-activating means for igniting said primer charge, said activating means extending from said squib through said casing and out the small end thereof, the inner end of said small cavity and the small end of said casing being substantially spaced from one another to provide a substantial body of combustible plastic therebetween.

Non-Radiating Extendible Cloth Exit Cone For Rocket Nozzles

US Patent:
4426038, Jan 17, 1984
Filed:
Jan 11, 1982
Appl. No.:
6/338713
Inventors:
Frank S. Inman - Brigham City UT
Joseph E. Pelham - Brigham City UT
Assignee:
Thiokol Corporation - Chicago IL
International Classification:
B64D 3304
US Classification:
23926515
Abstract:
A non-radiating cloth exit cone for a rocket nozzle includes a flared woven refractory cloth structure having the shape of the frustum of a cone with a refractory felt sewn to the exterior surface of the cloth structure for thermal insulation of the cloth structure and a sacrificial ablative material comprising tufts of refractory material incorporated in the interior surface of the cloth structure, the cloth structure providing the primary supporting structure for transmitting the rocket motor thrust forces to the rocket nozzle.

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