Static aerodynamic characteristics of a 1/9-scale model of the escape and exit configurations of the Project Mercury spacecraft at Mach numbers from 2.30 to 4.65, by Roger H. Fournier et al.

Title:	Static aerodynamic characteristics of a 1/9-scale model of the escape and exit configurations of the Project Mercury spacecraft at Mach numbers from 2.30 to 4.65
Author:	Fournier, Roger H.
Author:	Langley Research Center
Note:	National Aeronautics and Space Administration, 1962

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Subject:	Emergency vehicles -- Stability -- Testing
Subject:	Project Mercury (U.S.) -- Safety measures -- Testing
Subject:	Space vehicles -- Atmospheric entry
Subject:	Survival and emergency equipment -- Stability -- Testing
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