Jupiter atmospheric entry mission study. Volume 1 - Management summary Final report
Management summary and technical requirements for Jupiter atmospheric entry mission in 1978 using TOPS or Pioneer F/G spacecraft
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Problems of atmospheric entry
Aerodynamic and heating problems of spacecraft entry into Mars and Venus atmospheres
Bobbitt, P. J.↗
Flight dynamics of a straight wing space shuttle booster during entry
Dynamic flight control simulation for straight wing space shuttle booster entry
Kimbrel, L. G.↗
Hypersonic aerodynamic characteristics of DL-4 lifting entry vehicle
Analysis of aerodynamic forces on DL-4 lifting entry vehicle and comparison with theoretical methods
Ladson, C. L.↗
Extreme density profiles for Skylab command module entry considerations
Atmospheric density models for 30 N latitude for January and July for use in entry studies of Skylab command module
Pitts, D. E.↗
Imperfection sensitivity of optimum structural designs for a Mars entry capsule
Analytical evaluation of buckling modes of shell configurations to determine imperfection sensitivity of optimum structural designs for Mars entry capsule
Cohen, G. A.↗
Transonic aerodynamic characteristics of the Viking entry and Lander configurations
Wind tunnel tests to determine aerodynamic characteristics of Viking spacecraft entry and lander configurations at transonic speed
Mc Ghee, R. J.↗
Optimal lateral guidance for low L/D shuttle vehicle entry
Technique for designing switching thresholds in lateral guidance of entry vehicle
Deyst, J. J.↗
Approximate Optimal Atmospheric Entry Trajectories
Approximate optimal atmospheric entry trajectories maximizing terminal function of velocity, heading angle, flight path angle, and altitude
Speyer, J. L.↗
Preliminary analysis of an atmosphere-entry probe mission to Jupiter
Preliminary feasibility of depositing atmospheric entry probe from flyby mission to Jupiter
Swenson, B. L.↗
A study of a Jupiter atmospheric entry probe mission. Volume 1: Mangement summary
Science and engineering tradeoffs for Jupiter atmospheric entry probe mission
Winkler, H. B.↗
Hypersonic transitional and turbulent flow studies on a lifting entry vehicle
Hypersonic lifting entry vehicle turbulent heat transfer and boundary layer transition at various angles of attack and Reynolds numbers
Reda, D. C.↗
Estimation of the maximum temperature of a swept leading edge for an equilibrium glide entry
Maximum stagnation temperature on swept wing leading edge for equilibrium glide entry of space shuttle
Crawford, D. H.↗
Advanced high-power arc heaters for simulating entries into the atmospheres of the outer planets
High enthalpy electric arc plasma jet heaters for simulating entries in hydrogen rich Jovian atmosphere
Shepard, C. E.↗
Planetary entry body heating rate measurements in air and Venus atmospheric gas up to T equals 15,000 deg K
Convective plus radiative shock tube model stagnation point heating rate measurements for planetary entry heating rate in air and Venus gas
Livingston, F. R.↗
A study of a Jupiter atmospheric entry probe mission to the base of the cloud layers
Jupiter atmospheric entry probe missions to cloud layers base, discussing tradeoffs between various types of mission trajectories and technologies
Fields, D. P.↗
A Jupiter atmospheric entry mission
Jupiter atmospheric entry probe mission, discussing descent depths, atmospheric pressure and temperature effects, data return techniques and Grand Tour Missions
Carroll, P. C.↗
Optimal lateral guidance for low L/D shuttle vehicle entry
Optimal lateral guidance switching thresholds for low L/D shuttle vehicle entry, using optimal stochastic control theory for problem formulation in conjunction with dynamic programming
Deyst, J. J.↗