Contact Us

General Inquiry: Associate Director, Engineering Directorate
Phone: 281.483.8991
Email: jsc-ea-partnerships@mail.nasa.gov

Mailing Address:
National Aeronautics & Space Administration
Johnson Space Center
Mail Code: EA
2101 NASA Parkway
Houston, Texas 77058

JSC Engineering Web Address:
jsceng.nasa.gov

Test Facilities Guide

Engineering Test Facilities Guide

Download the Engineering Test Facilities Guide (PDF).

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Partners In

ISS with blue sky

International Space Station

Space Station Collaborators

Robotics and Human Hand

Technology Transfer

Innovative Partnerships Program (IPP)

Flight Mechanics Laboratory

    Flight Mechanics LaboratoryFlight Mechanics Laboratory
    Photo credit: NASA

    The Johnson Space Center Flight Mechanics Laboratory (FMLab) was organized in 1985 to build upon the mainframe-based computer analysis techniques developed early in the U.S. Space program and to continue and expand these computer analysis techniques using modern computer workstations. Presently the FML consists of 13 workstations with access to the JSC Cray Supercomputer and over 80 specially-developed software tools. The users include over 20 engineers experienced in various astrodynamics disciplines.

    Photo credit: NASA

    The FMLab is an internationally-recognized, world-class laboratory providing support to JSC, NASA, and the U.S. aerospace community for the development of orbital and interplanetary space missions.   The FMLab provides JSC with the facilities, hardware, software, techniques, and personnel to perform complete end-to-end performance analyses of exploration missions, future spacecraft, and on-going programs.  The FML values state-of-the-art computer systems, in-house development of analysis tools, engineers with world-class credentials, and quality service for laboratory customers.

    Work disciplines in the FMLab include the following:

    Ascent and Entry

    • Optimum performance
    • Preliminary guidance design
    • Monte Carlo analysis
    • Launch and landing opportunities
    • Preliminary control system design
    • Aerodynamic stability
    • Parachute deploy through landing dynamics

    Orbit

    • Mission design
    • Navigation analysis
    • Rendezvous design
    • Proximity operations
    • Two-body interaction

    Interplanetary

    • Mission planning
    • Trajectory design
    • Vehicle performance optimization
    • Launch and landing opportunities
    • Navigation analysis

Technical Point of Contact

Facility Documentation

Featured Engineering Projects