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This phase can take 3 to 4 minutes (for a solid rocket shorter than for a liquid-propellant rocket), the altitude at the end of this phase is 150–200 km, and the typical burn-out speed is 7 km/s.
Reimers was also a popular narrator of industrial films, especially those made by Lockheed Space and Missile Systems Division, Sunnyvale, California, and by the Aerojet-General Corporation Solid Rocket Plant in Sacramento, California.
The J-I was a solid rocket expendable launch vehicle developed by the National Space Development Agency of Japan and the Institute of Space and Astronautical Science.
The legacy of its lighter graphite-wound solid rocket motor technology lived on in the GEM side boosters used on the Delta rockets, and the Orion stages of the Pegasus air-launched rocket.
He began working with Oracle in 1990 at the Advanced Solid Rocket Motor Plant in Iuka, Ms. He is currently employed by Texas Memory Systems.
The Orion Abort Test Booster (ATB) is a small solid rocket launcher which will be developed by Orbital Sciences Corporation under contract by U.S. Air Force Space and Missile Systems Center, Space Development and Test Directorate (SDTD).
But because of the need to keep costs down and to allow President Richard Nixon to approve the shuttle program in 1972, NASA decided to utilize segmented solid rocket boosters similar to those used on the Titan III rocket instead of the S-IC, thus ending the Saturn program after the initial Saturn V order was completed.
When scientists at the Jet Propulsion Laboratory discovered that Thiokol's polymers made ideal binders for solid rocket fuels, Thiokol moved into the new field, opening laboratories at Elkton, Maryland, and later production facilities at Elkton and at Redstone Arsenal in Huntsville, Alabama.
Many Tracking and Data Relay Satellites were launched in the 1980s and 1990s with the Space Shuttle and made use of the Inertial Upper Stage, a two-stage solid rocket booster developed for the shuttle.