Benigno M Muniz

age ~66

from Venice, CA

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Also known as:

Benito Muniz
Uniz X Benigno
Benigno Cusick
Ben Muniz
Muniz Benigno

Connected to:

Benigno Muniz Phones & Addresses

Venice, CA
San Pedro, CA
600 Tivoli Psge, Alexandria, VA 22314 • 7035355751
Simi Valley, CA
Canoga Park, CA
Long Beach, NY
Los Angeles, CA
600 Tivoli Psge, Alexandria, VA 22314

Work

Company:

International launch services
May 2007
Position:

Program development director

Education

Degree:

Graduate-level Certificate
School / High School:

University of California, Los Angeles
1991 to 1998
Specialities:

Astronautical Engineering

Skills

Program Management • Systems Engineering • Aerospace • Engineering Management • Space Systems • Proposal Writing • Project Management • Integration • Spacecraft • Engineering • Strategic Planning • Strategy • Government • Satellite • Business Development • Systems Integration • International Project Management • Launch Vehicles • New Business Development • Capture Management • Competitive Assessments • Aircraft • Analysis • Requirements Management • Testing • Management • Leadership • Cross Functional Team Leadership • Statement of Work and Contract Negotiati... • Subsystems Engineering • Commercial • Technical Writing • Competitive Analysis • Simulations • Requirements Analysis • Aviation • Microsoft Project • Microsoft Office • Launch and on Orbit Operations • Startup Company • Proposal Management • Technical Communication • Competitive Technical Intelligence • Modeling and Simulation • Finite Element Modeling and Analysis • Structural Dynamics • Structural Dynamics Testing • Aeroservoelastic Analysis

Languages

English • Spanish • Russian

Ranks

Certificate:

U.s. Citizen

Interests

Padi Advanced Open Water • Scuba Diving • Padi Open Water

Industries

Defense & Space

Resumes

Senior Principal Engineer And Systems Engineering Lead

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Location:

924 Victoria Ave, Venice, CA 90291

Industry:

Defense & Space

Work:

International Launch Services since May 2007
Program Development Director
Constellation Services International, Inc. Jun 2000 - May 2007
Chief Technical Officer/Deputy Program Manager
Hughes Space & Communications Co., Space Systems Architecture group Nov 1995 - Jun 2000
Senior Staff Engineer
Rocketdyne Division/Rockwell Intl., System Engineering, Integration and Operations Product Area Apr 1990 - Nov 1995
Engineering Specialist
Grumman Aerospace Corporation Mar 1982 - Nov 1990
Loads and Dynamics Engineer

Education:

University of California, Los Angeles 1991 - 1998
Graduate-level Certificate, Astronautical Engineering International Space University 1994 - 1994
Certificate with Honors, Space Systems Architecture and Mission Design Clarkson University 1976 - 1981
BS, Mechanical Engineering

Skills:

Program Management
Systems Engineering
Aerospace
Engineering Management
Space Systems
Proposal Writing
Project Management
Integration
Spacecraft
Engineering
Strategic Planning
Strategy
Government
Satellite
Business Development
Systems Integration
International Project Management
Launch Vehicles
New Business Development
Capture Management
Competitive Assessments
Aircraft
Analysis
Requirements Management
Testing
Management
Leadership
Cross Functional Team Leadership
Statement of Work and Contract Negotiations
Subsystems Engineering
Commercial
Technical Writing
Competitive Analysis
Simulations
Requirements Analysis
Aviation
Microsoft Project
Microsoft Office
Launch and on Orbit Operations
Startup Company
Proposal Management
Technical Communication
Competitive Technical Intelligence
Modeling and Simulation
Finite Element Modeling and Analysis
Structural Dynamics
Structural Dynamics Testing
Aeroservoelastic Analysis

Interests:

Padi Advanced Open Water
Scuba Diving
Padi Open Water

Languages:

English
Spanish
Russian

Certifications:

U.s. Citizen
Basic Open Water Scuba Diving, Advanced Open Water Scuba Diving
Lsu L1 (Basic "Nitrox") Scuba Diving

Us Patents

Method And Apparatus For Supplying Orbital Space Platforms Using Payload Canisters Via Intermediate Orbital Rendezvous And Docking
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US Patent:

20030164428, Sep 4, 2003
Filed:

Mar 7, 2002
Appl. No.:

10/093971
Inventors:

David Anderman - Laguna Hills CA, US
Benigno Muniz - Simi Valley CA, US
Assignee:

Constellation Services International, Inc. - Woodland Hills CA
International Classification:

B64G001/62
US Classification:

244/161000
Abstract:

In a space platform supply system, a canister containing supply for a space platform is launched into orbit using a launch vehicle. An intermediate space vehicle rendezvous and docks with the canister while the attached launch vehicle provides the necessary orbit maintenance and stabilization to enable the docking. After docking, the intermediate space vehicle detaches the canister from the launch vehicle element or the launch vehicle element may initiate detachment from the intermediate space vehicle/canister. In either event, the intermediate space vehicle then can provide propulsion and attitude control to allow the canister to be transported to and docked with the space platform being supplied, thus eliminating the need for the canister to include propulsion and attitude control of its own.

Method And Apparatus For Supplying Orbital Space Platforms Using Payload Canisters Via Intermediate Orbital Rendezvous And Docking
view source
US Patent:

20050067534, Mar 31, 2005
Filed:

Dec 29, 2003
Appl. No.:

10/748527
Inventors:

David Anderman - Laguna Hills CA, US
Benigno Muniz - Simi Valley CA, US
Assignee:

Constellation Services International, Inc. (a Delaware corporation) - Woodland Hills CA
International Classification:

B64G001/62
US Classification:

244161000
Abstract:

In a space platform supply system, a canister containing supply for a space platform is launched into orbit using a launch vehicle. An intermediate space vehicle rendezvous and docks with the canister while the attached launch vehicle provides the necessary orbit maintenance and stabilization to enable the docking. After docking, the intermediate space vehicle detaches the canister from the launch vehicle element or the launch vehicle element may initiate detachment from the intermediate space vehicle/canister. In either event, the intermediate space vehicle then can provide propulsion and attitude control to allow the canister to be transported to and docked with the space platform being supplied, thus eliminating the need for the canister to include propulsion and attitude control of its own.