J. Marroquin

发表

Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman Gas Dynamics Facility (VKF) 40" supersonic and the 50" hypersonic wind tunnels A and C

J. Marroquin, C. R. Leef, 1985 .

Effects of reaction control system jet simulation on the stability and control characteristics of a 0.015 scale space shuttle orbiter model tested in the Langley Research Center unitary plan wind tunnel

J. Marroquin, J. J. Daileda, 1974 .

Results of wind tunnel RCS interaction tests on a 0.010-scale space shuttle orbiter model (51-0) in the Calspan Corporation 48-inch hypersonic shock tunnel (test 0A93)

J. Marroquin, J. J. Daileda, C. E. Rogers, 1976 .

Results of the AFRSI detailed-environment test of the 0.035-scale SSV pressure-loads model 84-0 in the Ames 11x11 ft. TWT and the Lewis 8x6 ft. and 10x10 ft. SWT (OA-310A, B, C), volume 1

J. Marroquin, B. A. Marshall, 1984 .

Results of SRB separation tests using the 0.010-scale SSV model 75-OTS in the AEDC VKF tunnel A(IA142), volume 1

J. Marroquin, J. J. Daileda, 1977 .

Results of a M = 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/Ames Research Center 3.5-foot hypersonic wind tunnel

J. Marroquin, 1985 .

Results of the AFRSI rewaterproofing systems screening test in the NASA/Ames Research Center (ARC) 2 x 2-foot transonic wind tunnel

J. Marroquin, R. B. Kingsland, 1985 .

Results of tests using a 0.0125-scale model (70-QT) of the space shuttle vehicle orbiter in the AEDC VKF tunnel B (IA22), volume 2

J. Marroquin, J. J. Daileda, 1977 .