EDGAR CASTRO
Electrician at Antoine Dr, Houston, TX

License number

Texas 161541

Expiration Date

Jun 1, 2017

Professional information

Business Change Manager North America Gas And Power At Bp

Position:

Business Change Manager North America Gas and Power at BP

Location:

Houston, Texas Area

Industry:

Oil & Energy

Work:

BP since Mar 2011 - Business Change Manager North America Gas and Power BP Apr 2010 - Mar 2011 - Middle Office Manager North America Gas and Power BP Aug 2008 - Apr 2010 - Head Global Gas SPU Performance and Planning - London- England BP Mar 2007 - Aug 2008 - Trade Control Manager UK Crude - London-England BP Aug 2005 - Mar 2007 - Performance and Control Manager - Financial Products BP May 2004 - Aug 2005 - Performance and Control Manager NGLs American Electric Power Jan 2002 - May 2004 - Senior Risk Analyst

Education:

Texas State University-San Marcos 1999 - 2001
Universidad del Valle (CO) 1991 - 1996
Chemical Engineer, Engineering

Chief, Structures At Nasa - Jsc - Es

Position:

Chief, Structures at NASA - JSC - ES

Location:

Houston, Texas Area

Industry:

Government Administration

Work:

NASA - JSC - ES - Chief, Structures

Edgar Castro - Houston, TX

Work:

Hotel city express PUEBLA angelopolis - Puebla de Zaragoza, Pue.
Hotel group and banquet coordinator

Education:

Benemrita universidad autnoma de Puebla - Puebla de Zaragoza, Pue.
Licensed in Hotels and hospitality industry

Skills:

Organization, honesty, arranging chairs and tables in the halls for private events

Pre-Integrated Truss Space Station And Method Of Assembly

US Patent:

5407152, Apr 18, 1995

Filed:

Dec 24, 1992

Appl. No.:

7/996763

Inventors:

Timothy E. Pelischek - League City TX
Edgar O. Castro - Houston TX
Gregg A. Edeen - Friendswood TX
David A. Hamilton - Houston TX
Jon B. Kahn - League City TX
James B. McDede - League City TX
Kornel Nagy - Houston TX
John V. Rivers - Houston TX
Irene E. Verinder - Dickinson TX
Donald C. Wade - Friendswood TX
Clarence J. Wesselski - Alvin TX

Assignee:

The United States of America as represented by the Administrator of
National Aeronautics & Space Administration - Washington DC

International Classification:

B64G 110

US Classification:

244159

Abstract:

The present invention is directed to methods and apparatus relating to design, construction, integration and assembly of a space station. The present invention uses pre-integrated open (unpressurized) truss segments for modular construction of the space station. Each segment includes a truss structure and utility subsystems which may be fully assembled and tested on Earth. The segments may be latched together on orbit using a remote latching system. Utility subsystems, such as solar panels and radiators, are pre-integrated into the appropriate truss segment, and are deployable from the respective truss segment on orbit. Rails run lengthwise along the assembled truss. The rails may be used with a mobile transporter for translating truss segments with respect to the spacecraft as part of the space station assembly process. The rails may also be used with a mobile transporter for carrying crew personnel, a robotic arm, and other equipment.

Heavy-Lift Vehicle-Launched Space Station Method And Apparatus

US Patent:

5441221, Aug 15, 1995

Filed:

Dec 3, 1993

Appl. No.:

8/161038

Inventors:

Donald C. Wade - Friendswood TX
Horacio M. De La Fuente - Friendswood TX
Reginald B. Berka - Houston TX
Steven L. Rickman - League City TX
Edgar O. Castro - Houston TX
Kornel Nagy - Houston TX
Clarence J. Wesselski - Alvin TX
Timothy E. Pelischek - Santa Fe TX
John A. Schliesing - Houston TX

Assignee:

The United States of America as represented by the Administrator of the
National Aeronautics and Space Administration - Washington DC

International Classification:

B64G 160, B64G 122, B64G 144

US Classification:

244159

Abstract:

Methods and apparatus are provided for a single heavy-lift launch to place a complete, operational space station on-orbit. A payload including the space station takes the place of a Shuttle Orbiter using the launch vehicle of the Shuttle Orbiter. The payload includes a forward shroud, a core module, a propulsion module, and a transition module between the core module and the propulsion module. The essential subsystems are pre-integrated and verified on Earth. The core module provides means for attaching international modules with minimum impact to the overall design. The space station includes six control moment gyros for selectably operating in either LVLH (local-vertical local-horizontal) or SI (solar inertial) flight modes.