Spacecraft and stage-geometry effects on the hypersonic characteristics of a horizontal- take-off reusable booster (1963)
Clark, L. R., Pierpont, P. K · leaf 15
UNCLASSIFIED WHfHRC!" Winqed-rockel spacecraf Plan view … Piggyback position ;7"Y-V-_-, - Underslunq positio (a) General arrangement of horlzontal-take-off-and-horlzontal-landing reusable booster system. Figure 1.- Arrangement and geometric details of horizontal-take-off-and-horlzontal-landing launch vehicle. All linear design dimensions are in inches. Ik…
Gas 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.
