Water impact test of aft skirt end ring, and mid ring segments of the space shuttle solid rocket booster
By: prepared by Structures and Mechanics Department, Chrysler Corporation, Electronics Products Division, Engineering Office, Michoud Assembly Facility for National Aeronautics and Space Administration, George C. Marshall Space Flight Center.
Contributors: Michoud Assembly Facility (Chrysler Corporation); George C. Marshall Space Flight Center.
Series: Technical note -- TN-SM-83-13.; NASA-CR -- 171027.; Technical note (Michoud Assembly Facility (Chrysler Corporation)) -- TN-SM-83-13.; NASA contractor report -- NASA CR-171027.
Publisher: The Center
Published: 1983
Place of publication: Huntsville, Ala
Language: eng
Format: Microform
Subjects: Rocket engines -- Thrust.
Notes: "September 1983."

"Test report for MSEC test #83-3."

"Contract NAS8-35017."

"N84-25752"--Microfiche header.

Includes bibliographical references.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1984]. 3 microfiches ; 11 x 15 cm.