OPTIMAL LOW-THRUST NEAR-CIRCULAR ORBITAL TRANSFER
Study of optimum low-thrust transfers between neighboring coplanar circular orbits for a simplified system model
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Study of optimum low-thrust transfers between neighboring coplanar circular orbits for a simplified system model
Manned space vehicle reentry at circular to hyperbolic velocities, considering deceleration, corridor width, heating, heat protection, vehicle weight, lateral ranging, and landing factors
Resonant bending frequencies and mode shapes for thin, circular cylindrical shell containing an internal liquid with a free surface
Buckling load of circular cylindrical shells under axial compression
Solutions for knudsen flow flux distributions with particles entering circular tube through small axial orifice - rocket thrustor application
Stressed and deformed state of stiffened circular cylindrical shell acted upon by transverse pressure and uniform axial loads
Fortran ii computer program for evaluation of donnell type differential equation for orthotropic circular-conical shell
Computer analysis of problems of four circular- coil system
Circular arrays for spacecraft antennas
High temperature circular aperture black body radiation source for field calibration of missile and airborne radiometers
Cavitation indices for circular pipe bends using water as working fluid
Transient heat transfer through thin circular pipe due to unsteady flow
Condition for swirling flow stability in circular magnetic field - mathematical analysis
Pressure distribution near single axial supply hole of externally pressurized circular thrust bearing - investigation of entrance effects
Oscillating air pressures within cylindrical chamber containing sinusoidally driven circular piston on end wall
Hyperspheroidal differential equation for circular mirror optical resonator modes for large and small Fresnel numbers
Density field for free molecule flow through circular ducts assuming steady state Maxwellian velocity distribution
Preformed metal strip, coiled flat on a storage drum, unrolls to form a cylindrical boom. Tabs and slots on opposite sides of the strip interlock to form a continuous circular cross section. This retractable boom can be used as a spacecraft antenna, gravity gradient, or positioning device.