A feasibility study for Scout polar launches from NASA Wallops Flight Center, Volume 2555
National Aeronautics and Space Administration, 1975 - Science - 31 pages
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1111 KM CIRCULAR achieve polar orbit Altair MlA altitude orbit Antares MB Atlantic Ocean impact Bahama lslands Black Brant boost yaw maneuver burnout Castor circular polar orbit Cons weight DRAG COEFFICIENT Elliptical polar orbit flight profile ft2 TABLE GROUNDTRACK heatshield HTPB impact area impact dispersion areas improved Scout configuration inert KM CIRCULAR ORBIT launch azimuth launched from NASA launched south lb Prop weight lb Total weight lbf-sec MB with XLDB mode of flight n.mi NASA Wallops Flight nautical mile Navy mission Ocean impact trajectory Orbit inclinations Pacific Ocean impact paragraph 2.2 payload weight capability polar orbit performance propellant remaining lb ROCKET ENGINE DATA Santiago de Cuba Scout F-1 second stage boost second stage impact shown in Figure Specific impulse stage boost yaw stage coast stage impact location stage yaw maneuvers third stage impact Vandenberg AFB vehicle hardware Wallops Flight Center weight Time sec yaw angle yaw rate steps yaw-torque