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An Analysis of Aerodynamic Requirements for Coordinated
Requirements Study for a Trident II Accuracy Evaluation System 40
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ablation acceleration aerodynamic air target airframe analysis angle angle of attack antenna areas autopilot Blum CBTT CBTT control ceramic chip carriers channel chip carriers command configuration data acquisition defense developed display dither effects electronic elliptical energy environment error estimate evaluation Figure film filter flight flow fluorometers frequency function geothermal Geothermal Energy graphite guidance Harpoon missiles heat Hopkins APL Tech inertial instrumentation interface JHU/APL Johns Hopkins APL Laboratory launch M-on-N model magnetic magnetometer maneuver measurements missile modulator monitor Naval NDPT oceanographic operating optical output parameters performance Pershing phase problem Proc processing processor pulse radar range roll sample satellite SATRACK scramjet sensor ship shown in Fig sideslip signal simulation singlet oxygen Standard Missile station supported surface switch tube tactical TCNQ temperature thermal Threat Upgrade tion track unit Univ vehicle velocity VIKING satellite voltage weapon system wire bond