[sci.space.shuttle] Final Shuttle motor joint test scheduled at Morton Thiokol

yee@ames.arc.nasa.gov (Peter E. Yee) (07/01/88)

Sarah Keegan
Headquarters, Washington, D.C.                     July 1, 1988
(Phone:  202/453-8536)

Ed Medal
Marshall Space Flight Center, Huntsville, Ala.
(Phone:  205/544-0034)


RELEASE:  88-86

FINAL SHUTTLE MOTOR JOINT TEST SCHEDULED AT MORTON THIOKOL


     Morton Thiokol, NASA's prime contractor for the Space 
Shuttle solid rocket motor, will conduct the seventh Joint 
Environment Simulator (JES) test Sunday, July 3, 1988, at 3:00 
p.m. EDT, at its Space Operations facility in Utah.  The test is 
part of the Space Shuttle solid rocket motor redesign program and 
is the final such test required prior to resumption of Shuttle 
flights.

     JES tests are short-duration, ignition pressure tests using 
full-scale motor hardware to form two field joints.  The tests 
are used to evaluate the redesigned joints.

     This test article, designated JES-3C, will be extensively 
flawed, including a wave-type defect in the J-seal bonded 
insulation of joint A, plus intentional channel-like defects 
through the J-seal in both joints.  In addition, the capture 
feature O-ring will be flawed in joint A and both the capture 
feature and primary O-rings will be flawed in joint B.  The 
defects are intended to ensure hot gas flow reaches the primary 
O-ring in joint A and the secondary O-ring in joint B.  This will 
allow engineers to verify the performance of the O-ring seals 
under hot gas conditions.

     The field joints also have both intentional and natural edge 
unbonds, some of which have been repaired.  The test will allow 
engineers to evaluate the effect of existing unbonds and also to 
evaluate the effectiveness of unbond repair procedures.  
Deliberate flaws also will be introduced in some of the primary 
seals in the motor igniter.


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     About 385 pounds of live propellant are used in a JES test 
to provide hot gas to duplicate the ignition pressure buildup of 
a full-size motor.  For this test, hot gas and pressure will be 
retained inside the test article and not allowed to vent until 
about 2 minutes after ignition.  This simulates full-duration 
motor conditions.



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