Experiments to determine communication capability of the echo ii satellite
Echo II satellite communication capability
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Echo II satellite communication capability
Echo II satellite observational data showing no change in apparent cross section one year after launch
Experiments with Echo II satellite to determine its capability as passive communications device and study shape and surface as function of time
Design, fabrication, packaging, and test methods used in Echo II satellite
Signal transmission from U.S.S.R. to United Kingdom via Echo II communications satellite
Radio beacon telemetry system for measuring orbital performance of Echo II satellite, including internal pressure and skin temperature
Beacon telemetry system for Echo II passive communications satellite
Performances of Echo II passive satellite, and passive satellite communications system
Communication satellites - echo i, echo ii, score, courier, telstar, relay and syncom
Membrane analysis of very thin pressurized spheroid shells composed of flat gores - application to Echo II satellite
Prototype ground spheres, television and beacon telemetry system, and communication experiments for Echo II satellite
Passive communication satellite theory - Echo I AND Echo II satellite applications
Photogrammetry method and analysis for determining strains in skin of Echo II passive communications satellite in prelaunch static inflation test
Echo ii communications satellite launching
Signal fading characteristics of Echo II SATELLITE - fade duration, and fade period probability distribution and density functions at various cross section levels
Statistical reduction of satellite effective radio cross section of reflected radio signal power measurements made on Echo I passive satellite
A general derivation is given for the earth reflected solar radiation input to a flat plate--a solar cell paddle, for example--which is spinning about an axis coincident with the axis of symmetry of the satellite to which it is affixed. The resulting equations are written for the general case so that arbitrary orientations of the spin axis with respect to the earth-satellite line and arbitrary orientations of the normal to the plate with respect to the spin axis can be treated. No attempt is made to perform the resulting integrations because of the complexity of the equations; nor is there any attempt to delineate the integration limits for the general case. However, the equations governing these limits are given. The appendixes contain: the results, in graphical form, of two representative examples; the general computer program for the calculation is given in Fortran notation; and the results of a calculation of the distribution of albedo energy on the proposed Echo II satellite. The value of the mean solar constant used is 1.395 times 10 (sup 4) ergs per centimeters-squared per second; the mean albedo of the earth is assumed to be 0.34; and the earth is assumed to be a diffuse reflector.
Echo II program to launch passive communications satellite that will maintain spherical shape and surface smoothness after loss of inflatant pressure