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Spacecraft and stage-geometry effects on the hypersonic characteristics of a horizontal- take-off reusable booster (1963)
Clark, L. R., Pierpont, P. K · leaf 19
UNULAbbiritu … L-62-6i+i7 (d) Long second-stage booster with winged-rocket spacecraft mounted above first-stage reusable booster. L-62-61+00 (e) Long second-stage booster with winged-rocket spacecraft mounted beneath first-stage reusable booster. Figure 2.- Concluded. 18 mimsmsi^Mt 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.
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