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Gary E Joseph, 48North Hollywood, CA

Gary Joseph Phones & Addresses

North Hollywood, CA   

West Hollywood, CA   

Maumee, OH   

Toledo, OH   

Kent, OH   

3525 London St, Los Angeles, CA 90026    213-7058861   

Work

Company: TRIPOINT MEDICAL CENTER Address: 7590 Auburn Rd, Concord Twp, OH 44077 Phones: 440-3758100 (Phone)

Education

School / High School: Ohio University College Of Osteopathic Medicine 1993

Languages

English

Images

Emails

Mentions for Gary E Joseph

Career records & work history

Lawyers & Attorneys

Gary Joseph Photo 1

Gary Joseph - Lawyer

ISLN:
906081714
Admitted:
1978

Medicine Doctors

Gary Joseph Photo 2

Dr. Gary F Joseph, Madison OH - DO (Doctor of Osteopathic Medicine)

Specialties:
Emergency Medicine
Address:
6270 N Ridge Rd, Madison, OH 44057
440-4280280 (Phone)
4700 Rockside Rd Suite 535, Independence, OH 44131
866-9725265 (Phone) 216-6420903 (Fax)
TRIPOINT MEDICAL CENTER
7590 Auburn Rd, Concord Twp, OH 44077
440-3758100 (Phone)
Languages:
English
Education:
Medical School
Ohio University College Of Osteopathic Medicine
Graduated: 1993

Publications & IP owners

Wikipedia

Gary Joseph Photo 50

Usergary Joseph

User:Gary Joseph. From Wikipedia, the free encyclopedia. Jump to: navigation, search. This is a Wikipedia user page. This is not an encyclopedia article. ...

Us Patents

Satellite Propulsion And Power System

US Patent:
5417049, May 23, 1995
Filed:
Aug 21, 1991
Appl. No.:
7/748990
Inventors:
Robert L. Sackheim - Palos Verdes CA
Dale L. Hook - Rancho Palos Verdes CA
Gary W. Joseph - Torrance CA
Assignee:
TRW Inc. - Redondo Beach CA
International Classification:
B64G 126
F02K 928
US Classification:
60260
Abstract:
In the preferred embodiment of the invention, a cooled bipropellant thruster 70 for controlling the on-orbit position and orientation of a spacecraft is provided. The cooled bipropellant thruster 70 uses a liquid fuel and liquid oxidizer. The liquid fuel is decomposed in a first chamber 72 with a catalytic bed of decomposition material 74 and produces at least one reaction gas, which flows to the second reaction chamber 90. The second reaction chamber 90 is heated by the reaction gas, but is cooled by liquid oxidizer flowing through cooling passages 92, 94, 98, and 102, which brings the oxidizer into a heat exchange relationship with the second reaction chamber 90. During the heat exchange relationship, heat is transferred from the second reaction chamber 90 to the oxidizer and the oxidizer transforms into a gas. The gaseous oxidizer is fed into a second reaction chamber 90 to secondarily react with the reaction gas.

Satellite Propulsion And Power System

US Patent:
5572865, Nov 12, 1996
Filed:
Sep 1, 1994
Appl. No.:
8/299782
Inventors:
Robert L. Sackheim - Rancho Palos Verdes CA
Dale L. Hook - Rancho Palos Verdes CA
Gary W. Joseph - Torrance CA
Assignee:
TRW Inc. - Redondo Beach CA
International Classification:
F02K 968
US Classification:
60260
Abstract:
In the preferred embodiment of the invention, a cooled bipropellant thruster 70 for controlling the on-orbit position and orientation of a spacecraft is provided. The cooled bipropellant thruster 70 uses a liquid fuel and liquid oxidizer. The liquid fuel is decomposed in a first chamber 72 with a catalytic bed of decomposition material 74 and produces at least one reaction gas, which flows to the second reaction chamber 90. The second reaction chamber 90 is heated by the reaction gas, but is cooled by liquid oxidizer flowing through cooling passages 92, 94, 98, and 102, which brings the oxidizer into a heat exchange relationship with the second reaction chamber 90. During the heat exchange relationship, heat is transferred from the second reaction chamber 90 to the oxidizer and the oxidizer transforms into a gas. The gaseous oxidizer is fed into a second reaction chamber 90 to secondarily react with the reaction gas.

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