Simulation of total equilibrium shock-layer radiation for three typical entry body shapes.
Satellite system survival probability expressed as function of launch probability, time and number of satellites available
Dyner, H. B.↗
Engineering topics
Dyner, H. B.
Publications and source records attributed to Dyner, H. B..
Study of optical radiation in the wavelength regions of 0.4216 mu, 0.4278 mu, 0.4835 mu, and 0.5165 mu behind normal shock waves in a simulated Martian atmosphere
Optical radiation measurements behind shock wave in simulated Mars atmosphere
Arnold, J. O.↗
Simulation of total equilibrium shock layer radiation for three typical entry body shapes.
Total equilibrium shock layer radiation data for Martian entry body shapes at various angles of attack extrapolated to trajectory condition
EARTH-MARS RENDEZVOUS TRAJECTORY↗
An experimental comparison of three typical Mars entry body shapes on the basis of total equilibrium shock-layer radiation
Comparative study of total equilibrium shock layer radiation for three potential Mars entry body shapes
MARS /PLANET/↗