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
Author:   National Aeronaut Administration (Nasa)
Publisher:   Createspace Independent Publishing Platform
ISBN:  

9781724694966


Pages:   32
Publication Date:   06 August 2018
Format:   Paperback
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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


Overview

An experimental investigation was performed in the NASA/Ames Research Center 3.5-foot Hypersonic Wind Tunnel to obtain supersonic heat-distribution data in areas between the orbiter and external tank using phase-change paint techniques. The tests used Novamide SSV Model 56-OTS in the first and second-stage ascent configurations. Data were obtained at a nominal Mach number of 5.3 and a Reynolds number per foot of 5 x 10 to the 6th power with angles of attack of 0 deg, +/- 5 deg, and sideslip angles of 0 deg and +/- 5 deg. Marroquin, J. Unspecified Center NASA-CR-167695, NAS 1.26:167695, DMS-DR-2524 NAS9-17179

Full Product Details

Author:   National Aeronaut Administration (Nasa)
Publisher:   Createspace Independent Publishing Platform
Imprint:   Createspace Independent Publishing Platform
Dimensions:   Width: 21.60cm , Height: 0.20cm , Length: 28.00cm
Weight:   0.102kg
ISBN:  

9781724694966


ISBN 10:   1724694960
Pages:   32
Publication Date:   06 August 2018
Audience:   General/trade ,  General
Format:   Paperback
Publisher's Status:   Active
Availability:   Available To Order   Availability explained
We have confirmation that this item is in stock with the supplier. It will be ordered in for you and dispatched immediately.

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