On the decrease of the radar cross section of the Apollo command module due to reentry plasma effects
Apollo command module radar cross section decrease due to reentry plasma effects
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Apollo command module radar cross section decrease due to reentry plasma effects
Design evaluation of heat source array for isotope reentry vehicle
Indirect pilot viewing systems for reentry vehicles and SST, discussing overlapping monoculars and panoramic display
Space emergency reentry vehicle - NASA Faculty Systems Engineering Institute Conference, University of Houston, June-August 1967
Apollo antenna design before and after reentry, discussing radio blackout problems and S band helices performance
Optimal trajectory control of lifting reentry vehicle under measurement uncertainties
Synoptic density maps for post-reentry altitudes derived from constant pressure charts and horizontal gradients
Isotope reentry vehicle/Brayton cycle space power system design, noting blunt conical aeroshell housing of heat source capsule
Space to reentry environmental sequence simulator for heat shield materials uninterrupted vacuum transfer without exposure to atmosphere
Computer mechanization of reentry equations with four degrees of freedom
Vacuum ultraviolet detector-spectroscopy systems for capsule reentry measurements
Convective and radiative heat transfer during reentry simulation
Analysis of ground and flight tests for reentry experiments
Laminar heat transfer distributions for blunted- cone, cone frustum reentry configuration at hypersonic speed using Reynolds number
Measurements of mutual interference heating for probe antenna mounted on Apollo reentry configuration
Preliminary design and performance considerations for 25 kW Pu 238 heat source Isotope Reentry Vehicle
Mathematical models for low speed reentry guidance of Apollo vehicles
Atmospheric gas composition effects on shock layer radiative heat transfer and heat shield response in Venus entry simulated by earth reentry