| 000 | 00702 a2200241 4500 | ||
|---|---|---|---|
| 001 | 281162 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA TP 2307 : 1985 | ||
| 245 | _aExperimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal mach number of 7 | ||
| 250 | _a | ||
| 260 | _aWashington, D.C. | ||
| 260 | _bNational Aeronautics and Space Administration | ||
| 260 | _c1985 | ||
| 300 | _a48 p. | ||
| 300 | _c | ||
| 856 | _u | ||
| 490 | _aNASA TP 2307 : 1985 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aSpace shuttle, Hypersonic flow, Thermal protection, Reusable surface, Impingement heating | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c240612 _d240612 |
||