Static stability and drag characteristics of the HAST missile at Mach numbers 2.25, 3.0, and 4.0 /
J.T. Best, Jr. and R.W. Rhudy.

Description

Main Author

Best, J. T., Jr.

Related Names

Rhudy, R. W., author.
ARO, Inc.
Arnold Engineering Development Center
United States. Air Force.

Language(s)

English

Published

Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1974.

Subjects

Drag (Aerodynamics)
Guided missiles > Guided missiles / Aerodynamics.
Guided missiles > Guided missiles / Testing.

Summary

Static-force tests were conducted at Mach number 2.25, 3, and 4 on a 0.25 -scale model of the High Altitude Supersonic Target (HAST) missile.

Note

Report was prepared by ARO, Inc., a subsidiary of Sverdrup & Parcel and Associates, Inc.
"Final Report for Period September 4 -- 13, 1973."
"April 1974."

Physical Description

94 pages : illustrations, 28 cm

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