Bodies of constant stress experiencing forces of orbital flight
Bodies of constant stress experiencing orbital flight centrifugal and gravitational forces
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Bodies of constant stress experiencing orbital flight centrifugal and gravitational forces
Use of low constant thrust to accomplish orbital transfer
Variable time constant, wide frequency range smoothing network for noise removal from pulse chains
Solar constant and solar spectrum measured from research aircraft
Polycrystalline rocks elastic constant and nonelastic behavior, discussing Voigt, Reuss and Hill averaging methods
Thermoelectric-couple life tests and efficiency measurements at constant thermal input, noting insulation for limiting parasitic heat losses
Adiabatic elastic stiffness constants of single crystal forsterite measured as function of hydrostatic pressure and temperature, using pulse superposition technique
Constant thrust electric propulsion systems performance with coast trajectories presented for 100 AU extraecliptic missions
Electron-neutrino weak interaction and beat decay coupling constants found nearly equal, describing astrophysical tests based on white dwarf stars luminosity intervals
Methyl fluoride calculated for ion-molecule reaction rate constants from ion cyclotron resonance spectra
Rotational, vibrational and equilibrium molecular constants for Phillips system of diatomic carbon
Optimal constant output feedback gains for linear multivariable systems, noting control vector as time invariant function of output vector
Vibrational energies, rotational constants and internuclear potential of ground state molecular iodine, using reanalyzed spectroscopic data
Engineering standard for solar constant and zero air mass solar spectral irradiance from high altitude measurements
Closed form solution for minimum fuel constant thrust trajectories for vehicle transfer in vacuum between arbitrary boundary conditions
Single crystalline mercury elastic constants calculated from propagation velocity measurements of polarized sound waves
Linear micromorphic material constants determination from constituent properties based on microelasticity theory
Interplanetary trajectories calculation using constant and/or slowly varying functions for accuracy, noting application to earth-moon spacecraft