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Cross Range 2,419 km.Shuttle MDC-A-1 LOx/LH2 propellant rocket stage. Delta winged configuration.Shuttle MDC-A-2 LOx/LH2 propellant rocket stage. HL-10 lifting body configuration.Shuttle NAR A-1 LOx/LH2 propellant rocket stage. Faget Straight Wing Configuration....
Apogee: 1,419 km (881 mi). Perigee: 323 km (200 mi). Inclination: 81.00 deg. Period: 102.37 min. 3U cubesat which split after deployment into four spacer sections that released three 0.10 m diameter aluminium spheres used as passive atmospheric density calibration probes.. ...
8D419 -Manufacturer's designation of8D423N2O4-UDMH rocket engine. 8D420 -Article Number ofRD-270N2O4-UDMH rocket engine. 8D420M -Article Number ofRD-270MN2O4-Pentaborane rocket engine. 8D423-Izotov N2O4/UDMH rocket engine. Production from 1964. Single chamber engine for UR-100 stage 2. Gas...