Heat-transfer distributions on a 0.013-scale shuttle solid rocket booster at Mach 3.70 and angles of attack from 0 ̊to 180 ̊ /

Bibliographic Details

Main Author:	Lamb, Milton
Corporate Authors:	United States. National Aeronautics and Space Administration, Langley Research Center
Other Authors:	Stallings, Robert L.
Format:	Government Document Book
Language:	English
Published:	Washington : National Aeronautics and Space Administration ; 1976.
Series:	NASA technical memorandum ; NASA TM X-3417.
Subjects:	Rocket engines. Reusable space vehicles.