SRB/SLEEC (Solid Rocket Booster/Shingle Lap Extendible Exit Cone) feasibility study.
Subtitle: final report
By: prepared by Garrett Pneumatic Systems Division.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA-CR -- 178974.; NASA contractor report -- NASA CR-178974.
Publisher: National Aeronautics and Space Administration
Published: 1988
Place of publication: [Washington, DC
Language: eng
Format: Microform
Subjects: Space vehicles -- Propulsion systems.
Other titles: Design study for a SLEEC actuation system.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1988. 2 microfiches.