APA (7th ed.) Citation

Marroquin, J. (1985). 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 (IH-42). Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration.

Chicago Style (17th ed.) Citation

Marroquin, J. 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 (IH-42). Houston, Texas: Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, 1985.

MLA (9th ed.) Citation

Marroquin, J. 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 (IH-42). Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, 1985.