Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a Mach number of 2.01 / by Gerald V. Foster.

Author/creator Foster, Gerald V. author.
Other author United States. National Aeronautics and Space Administration issuing body.
Format Electronic
Publication[Washington, D.C.] : National Aeronautics and Space Administration, [November 1959]
Description1 online resource (24 pages) : illustrations.
Supplemental Contenthttps://purl.fdlp.gov/GPO/gpo182862
Subjects

SeriesNASA/TM ; X-134
NASA technical memorandum ; X-134. ^A467613
General noteGPO Cataloging Record Distribution Program (CRDP).
Bibliography noteIncludes bibliographical references (page 6).
Report noteTechnical memorandum.
Source of descriptionDescription based on online resource; title from PDF caption (NASA, viewed on May 26, 2022).
Issued in other formPrint version: Foster, Gerald V Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a mach number of 2.01
GPO item number0830-D (online)
Govt. docs number NAS 1.15:X-134