Preliminary analysis of an atmosphere-entry probe mission to Jupiter
Preliminary feasibility of depositing atmospheric entry probe from flyby mission to Jupiter
Engineering topics
Publications and source records attributed to Swenson, B. L..
Preliminary feasibility of depositing atmospheric entry probe from flyby mission to Jupiter
Atmospheric entry probe from flyby mission to Jupiter, considering descent trajectory feasibility and instrument package
Investigation of survivability of spacecraft components during entry of Jupiter atmosphere to determine probability of biological contamination
Orbital mechanics and observation tradeoffs for earth resources satellite
Launch windows for Mars departures from elliptical orbits and associated propulsive velocity requirements
Analysis of launch windows from circular orbits for representative Mars missions
Apollo command module, biconic and cone hyperbolic reentry vehicles engineering, discussing L/D ratio, heat protection and weight
Launch window variation using circular and elliptical parking orbits and transfer techniques, discussing Venus and Mars flyby missions
Elliptic capture orbits for missions to near planets
Lifting entry vehicles requirements for near earth and planetary missions, noting four thermal protection systems
Launch window analysis for round trip Mars missions
Lifting requirements of entry vehicles for near- earth planetary missions
Reentry flight corridor depth reduction as result of inadequate flight data at hyperbolic speeds, noting overshoot limit and inverted attitude
Problem of operational flexibility in Mars landing mission, discussing use of lifting vehicles
Reentry flight corridor depth reduction as result of inadequate flight data at hyperbolic speeds, noting overshoot limit and inverted attitude
Heating and heat-shield requirements for maneuverable, lifting body, entry vehicle