Inside Out Library · Explore
Spacecraft and stage-geometry effects on the hypersonic characteristics of a horizontal- take-off reusable booster (1963)
Clark, L. R., Pierpont, P. K · leaf 18
UNCLASSIFIED HiliMMi. (a) First-stage reusable booster. L-62-6U10 L-62-6U2O (b) Short second-stage booster with ballistic spacecraft mounted above first-stage reusable booster. … L-62-61+16 (c) Short second-stage booster with winged-rocket spacecraft and afterbody fairing mounted above first-stage reusable booster. Figure 2.- Photographs of first-stage reusable booster and launch vehicle with various upper-stage arrangements. 17 UNCLASSIFIEDGas lubricants · Gas turbine engines · Seals (stoppers) · Self sealing · Air breathing engines · Ceramics · Film thickness · Performance tests · Systems analysis
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
More pictures from Spacecraft and stage-geometry effects on the hypersonic characteristics of a horizontal- take-off reusable booster
More like this
![An illustration from Grundbegriffe Der Neuen Gestaltenden Kunst [Basic Concepts of the New Creative Art] (1925)](https://img.insideoutlibrary.com/img/200/ia-grundgegriffe-der-neuen-gestaltenden-kunst-doesburg-1925-62-0.webp)
![An illustration from Annual exhibition [electronic resource] : no jury, no prizes (1917)](https://img.insideoutlibrary.com/img/200/ia-bml-31072001518903-28-22.webp)
