Attitude stability of a spinning passive satellite in a circular orbit Semiannual technical progress report, Dec. 1, 1965 - May 31, 1966
Attitude stability of a spinning passive satellite in circular orbit
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Attitude stability of a spinning passive satellite in circular orbit
Predicting inversion load of circular tube
Transient heat transfer between thin circular tube and incompressible fluid, considering radial conduction and heat loss
Static pitching moment coefficient determination from location of center of pressure in right circular cone, using Newtonian impact mechanics
Nonlinear flexural vibrations of thin circular rings analyzed, using Galerkin procedure on motion equations
Attitude stability of spinning passive satellite in circular orbit
Test times and boundary layer induced property variations in circular shock tube
Nonlinear feedback solution for minimum-time injection into circular orbit with constant thrust acceleration magnitude
Frequency of free vibrations in circular conical shells
Rigorous solution to problem of stressed state of circular thick disk in field of centrifugal forces
Load carrying capacity of smooth circular cylindrical shells under compression
Central impact of external forces of axisymmetrical body on circular plate of uniform thickness
Dynamic stability of eccentrically reinforced circular cylindrical shells
Approximation method for determining critical load of unlimited circular planar body weakened by isolated crack
Lateral range requirements used in selecting spacecraft landing recovery sites for return from low circular orbits
Nonlinear flexural vibration analysis using Galerkin method in thin-walled circular cylinders
Optimal guidance equations for ascent trajectories into circular orbits, developing feedback guidance loop for real onboard control system
Preliminary circular orbit determination from single state of range-only data