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Manned Planetary Spacecraft
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BMAP_45261.png
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Portable Network Graphic
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1993-04-08
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5KB
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512x342
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1-bit (2 colors)
Labels:
text
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sketch
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drawing
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white
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diagram
OCR:
Basic Data L/D = 0.4 Y/CoA = 50 4-Man Cabin Docking Cone Heat Shield Diameter Ascent Prop. - OF2/MMH (2 Abreast) (Extended) - 544 in. ISP = 386 sec. Desc. Prop. Ascent Stage Attitude Control System Liquid - same as Ascent Solid - Isp = 310 sec Supersonic Parachutes Overall length - 360 in. "Ascent Propulsion Ablative Heat Shield Unsymmetrical to Mars Surface Living Quarters Obtain Lift Stowage for Rover Heat Shield Solid Landing Stowed Rockets (4) Heat Shield For Terminal Deployed for Impulse Deorbit & Hover Landing Liquid Propulsion Stage
