Press Release

New insulation design on Shuttle’s motor set for test Jan. 23 in Utah

By SpaceRef Editor
January 22, 2003
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An insulation design change that will further enhance the safety of the Space Shuttle’s Solid Rocket Motor nozzle is set for its final certification test on a static firing of a full-scale flight support motor Thursday, Jan. 23, at a Utah test facility. The test will help qualify new insulation designed to improve flight safety and reduce costs. The Reusable Solid Rocket Motor Project Office at Marshall tests motors annually to qualify any proposed upgrades or changes to the motor.

Photo: Static tests on Shuttle flight support motors are a key element of the “test before you fly” maxim of the Reusable Solid Rocket Motor Project Office. (ATK Thiokol)

An insulation design change that will further enhance the safety of the Space Shuttle’s Solid Rocket Motor nozzle is set for its final certification test on a static firing of a full-scale flight support motor Thursday, Jan. 23, at a Utah test facility.

Results from the test — to be conducted at the Promontory, Utah, facilities of ATK Thiokol Propulsion, an Alliant Techsystems Inc., company — will be used to qualify a new insulation design on the motor’s nozzle to case.

The new design will improve flight safety and help reduce costs on the motor, according to Jody Singer, project manager of the Reusable Solid Rocket Motor Project Office at NASA’s Marshall Space Flight Center in Huntsville, Ala.

Static — or stationary — firings of flight support motors are part of Shuttle’s ongoing verification of components, materials and manufacturing processes required by the Space Shuttle program. Flight support motors are tested annually to evaluate, validate and qualify any proposed upgrades or changes to the motor. The two-minute test duration is the same length of time that the motors perform during Shuttle flights.

On this motor, there are 97 objectives and a total of 459 instrumentation channels being tested. There are 10 principal objectives for the test of Flight Support Motor-10.

“Full-scale static testing is a key element in our program,” said Singer. “The rule is: Everything we fly, we static test first.”

The test will be conducted in the T-24 bay of the Thiokol test facility, north of Salt Lake City. Following the test, the data will be analyzed and the results for each objective provided in a final report. The metal case segments and nozzle components will be refurbished for reuse. 

At 126 feet (38.4 meters) long and 12 feet (3.6 meters) in diameter, the Shuttle’s Reusable Solid Rocket Motor is the largest solid rocket motor ever flown and the first designed for reuse. During its two-minute burn at liftoff, each motor generates an average thrust of 2.6 million pounds (1.2 million kilograms).

Marshall Space Flight Center has the responsibility for research, technology maturation, design, development, and integration for space transportation and propulsion systems. This includes both the reusable space transportation systems for Earth-to-orbit applications, as well as vehicles for orbital transfer and deep-space transportation.

NOTE TO EDITORS / NEWS DIRECTORS:  A special viewing area will be provided at Thiokol’s Utah test facility for the news media. To attend the firing, media representatives must register with Melodie deGuibert of Thiokol by telephoning (435) 863-3169 no later than 4 p.m. MDT Wednesday, Jan. 22.

Supporting materials for this news release — such as photographs, fact sheets, video and audio files and more — please visit the NASA Marshall Center Newsroom Web site at www.msfc.nasa.gov/news 

SpaceRef staff editor.