Design analysis - Unified S-band system for Apollo network, volume 3, part V /cont./ Engineering report
Design analysis of data demodulation equipment requirements for Apollo unified S-band ground tracking stations
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Design analysis of data demodulation equipment requirements for Apollo unified S-band ground tracking stations
Unified S-band telecommunication system for Apollo spacecraft-ground station communications
Unified S-band system for tracking and communicating with Apollo spacecraft during lunar mission
Unified treatment to predict turbulent fluxes in hot and multicomponent flows around launch vehicles
Apollo unified S-band system covering station locations, uplink and downlink spectrums, spacecraft gross parameters, theory of operation, etc
Unified approach to propagation of plane, cylindrical and spherical dilation waves in elastic media, using method of characteristics
Projection operators applicable for rearrangement and exchange processes with full recoil effect for unified reaction theory of Feschbach
Unified approach to propagation of plane, cylindrical and spherical dilation waves in elastic media, using method of characteristics
Unified S-band system in Apollo network to provide tracking and communications to lunar distance
Least squares analysis of unified S-band system high speed range rate and X-Y angular data from AS-202 mission
Multidisciplinary approach to unified information processing telemetry system
Unified approach to one-dimensional elastic waves by method of characteristics
Signal margin calculation procedures for CSM UNIFIED S-BAND downlink channel Apollo AS-202 TO aircraft NASA 432
Unified theory for galaxy spiral formation and radio galaxy and quasar evolutionary dynamics, discussing galactic dipole magnetic field generation
AS-204 signal reception predictions for unified S-band
Evaluation and performance analysis of unified S band system for Apollo ground network
Functional capabilities and physical arrangement of receiver exciter subsystem in unified S band Apollo communications and tracking ground station system
Unified form of Lambert theorem for elliptic, hyperbolic, and parabolic orbits based on selecting independent variable and normalized time of flight parameter