Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system / J.R. DeBonis and C.J. Trefny.

Author/creator DeBonis, James R.
Other author Trefny, Charles J.
Other author NASA Glenn Research Center.
Format Microform
Publication Info[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
Description1 volume.

SeriesNASA technical memorandum ; NASA/TM-2001-210567
NASA technical memorandum ; 210567. ^A467613
General noteShipping list no.: 2002-0157-M.
General noteCRDP Program record.
Reproduction noteMicrofiche. [Washington, D.C. : National Aeronautics and Space Administration, 2001?]. 1 microfiche.
Issued in other formPrint version: Supersonic Wind Tunnel Tests of a Half-Axisymmetric 12 Deg-Spike Inlet to a Rocket-Based Combined-Cyc
Issued in other formOnline version: DeBonis, James R. Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system
GPO item number0830-D (MF)
Govt. docs number NAS 1.15:210567
Stock number20010056686 NASA

Availability

Library Location Call Number Status Item Actions
Joyner Microforms B300 NAS 1.15:210567 ✔ Available