Search

Scott Matsunami Phones & Addresses

  • 12756 Caravel St, Cerritos, CA 90703 (818) 207-5438
  • Artesia, CA
  • 20043 Labrador St, Chatsworth, CA 91311 (818) 701-0349
  • Cincinnati, OH
  • Fullerton, CA
  • Los Angeles, CA
  • Lafayette, IN

Resumes

Resumes

Scott Matsunami Photo 1

System Engineering Architecture, Opscon, Interfaces, Integration And Trades Lead

View page
Location:
Los Angeles, CA
Industry:
Defense & Space
Work:
Northrop Grumman Aerospace Systems - Redondo Beach, CA since Oct 2003
System Integration Performance Assessment Project Manager

Raytheon Space and Airborne Systems - El Segundo, CA 2002 - 2003
System Engineering Manger

Boeing Satellite Systems - El Segundo, CA 1991 - 2002
Campaign Engineering Manager

Northrop Grumman Aerospace Systems - Redondo Beach, CA 1989 - 1991
Mechanical Design Integration Engineer - TDRSS

Pratt & Whitney - Canoga Park, CA 1987 - 1989
Design Engineer - Space Station
Education:
University of Missouri-Rolla 1980 - 1984
BSME, Mechanical Engineer
Skills:
Systems Engineering
Integration
Program Management
System Design
Requirements Management
Satellite
Space Systems
Spacecraft
Earned Value Management
Aerospace
Security Clearance
System Architecture
Proposal Writing
Defense
Military
Engineering Management
Sensors
Configuration Management
Dod
Engineering
Government Contracting
Process Improvement
Avionics
National Security
Six Sigma
Aircraft
Project Management
Systems Design
Cross Functional Team Leadership
Design
Mechanical Engineering
Interests:
Arts and Culture
Scott Matsunami Photo 2

Scott Matsunami

View page
Location:
Cerritos, CA

Publications

Us Patents

Agile, Spinning Spacecraft With Sun-Steerable Solar Cell Array And Method

View page
US Patent:
60682183, May 30, 2000
Filed:
May 14, 1997
Appl. No.:
8/855684
Inventors:
Christopher M. Cosner - Manhattan Beach CA
Scott M. Matsunami - Chatsworth CA
David L. Behrin - Culver City CA
Assignee:
Hughes Electronics Corporation - El Segundo CA
International Classification:
B64G 144
US Classification:
244173
Abstract:
An agile, spinning spacecraft has a first body portion and a second body portion which is rotatably coupled about a first rotational axis to the first body portion. A pair of planar solar cell arrays are rotatably coupled to the second body portion along a second rotational axis that is preferably orthogonal to the first rotational axis. The first body portion can be spun if desired and the first rotational axis can be directed by an attitude control system to have selected orientations. The solar cell arrays are rotated about the first and second rotational axes in accordance with steering laws which maintain the arrays in an orthogonal relationship with a Sun line.
Scott M Matsunami from Cerritos, CA, age ~62 Get Report