RICHARD ALLEN THOMPSON, PT
Restorative Service Providers in Huntsville, AL
License number
Alabama PTH553
Category
Restorative Service Providers
Type
Geriatrics
Address
Address
2
5275 Millennium Dr., Huntsville, AL 35806
107 Southwood Dr, Madison, AL 35758
107 Southwood Dr, Madison, AL 35758
Phone
(256) 489-6800
(256) 489-6520 (Fax)
(256) 830-2550
(256) 489-6520 (Fax)
(256) 830-2550
Professional information
Richard A Thompson, Huntsville AL - PT (Physical therapy)
Specialties:
Geriatric Medicine
Address:
5275 Millennium Dr NW, Huntsville 35806
(256) 489-6800 (Phone), (256) 489-6520 (Fax)
(256) 489-6800 (Phone), (256) 489-6520 (Fax)
Languages:
English
Liquid Fuel Expulsion System
US Patent:
4561568, Dec 31, 1985
Filed:
Mar 2, 1984
Appl. No.:
6/585704
Inventors:
Lawrence D. Hoffmeister - New Market AL
Jimmy M. Madderra - Huntsville AL
Richard J. Thompson - Huntsville AL
Jimmy M. Madderra - Huntsville AL
Richard J. Thompson - Huntsville AL
Assignee:
The United States of America as represented by the Secretary of the Army - Washington DC
International Classification:
B67D 542
US Classification:
222130
Abstract:
An explusion system in which an inner tank is nested within a second and er tank to provide a very compact and space saving arrangement for an expulsion system for a rocket with the first and inner tank as well as the second and outer tank being reinforced with composite material to provide a space saving and relatively light expulsion system for a rocket.
Method Of Making Rocket Motor Case With Integral Nozzle
US Patent:
4440587, Apr 3, 1984
Filed:
Aug 2, 1982
Appl. No.:
6/404253
Inventors:
Richard J. Thompson - Huntsville AL
Ocke C. Fruchtnicht - Huntsville AL
Ocke C. Fruchtnicht - Huntsville AL
Assignee:
The United States of America as represented by the Secretary of the Army - Washington DC
International Classification:
B32B 3100, B65H 5464
US Classification:
156154
Abstract:
A method of making a rocket motor case with an integral nozzle in which the rocket motor has a large length to diameter ratio and is made by applying a linear wrap of fibers as a first layer on a mandrel and then by applying radial wraps over said linear wrap and also conforming the linear fibers to the shape of the nozzle after applying the linear fibers on said mandrel to provide a structure that has sufficient stiffness to accomplish the desired result of a large length to diameter rocket motor case.
Lightweight Composite Launcher Pod Production Process
US Patent:
4556438, Dec 3, 1985
Filed:
Aug 20, 1984
Appl. No.:
6/642845
Inventors:
Lawrence D. Hoffmeister - New Market AL
Richard J. Thompson - Huntsville AL
Richard J. Thompson - Huntsville AL
Assignee:
The United States of America as represented by the Secretary of the Army - Washington DC
International Classification:
B31C 1300, B32B 518, B65H 8100
US Classification:
156 79
Abstract:
A process for making lightweight composite launcher pods in which a multicity of launcher tubes are wound on a multiplicity of mandrels and mounted in end structures of a mold and assembled into a generally rectangular mold structure and applying syntactic foam about the tube and spacer structure within the mold and finally curing the structure within the mold to provide a unitary lightweight composite launcher pod.
Lightweight Composite Launcher Pod
US Patent:
4604939, Aug 12, 1986
Filed:
Aug 20, 1984
Appl. No.:
6/642850
Inventors:
Lawrence D. Hoffmeister - New Market AL
Richard J. Thompson - Huntsville AL
Richard J. Thompson - Huntsville AL
Assignee:
The United States of America as represented by the Secretary of the Army - Washington DC
International Classification:
F41F 304
US Classification:
89 1816
Abstract:
A lightweight composite launcher pod which includes a multiplicity of eloted launcher tubes that are accurately aligned in a composite material with the composite material having four outer sides with alignment surfaces on three of the sides and bearing and alignment surfaces on the other side, and the lightweight composite launcher pod being capable of serving as the shipping and storage container for rockets before launching of the rockets as well as for launching the rockets therefrom when mounted in a launcher structure.