Landing impact attenuation for non-surface- planing landers
Landing impact attenuation for non-surface planing landers
Jones, R. H.↗
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Design and fabrication of a full-size landing impact test model of the Mars legged lander configuration Master agreement, task order three
Design and fabrication of full size landing impact test model of Mars legged lander configuration
Lopatin, A.↗
Evaluation of entry and terminal deceleration systems for unmanned Martian landers
Entry and terminal deceleration systems for unmanned Martian landers, discussing parachute landing and lifting entry vehicles
Harrison, E. F.↗
Thermal death of Bacillus subtilis var. niger spores on selected lander capsule surfaces
Dry heat resistance of bacillus subtilis var. niger spores on selected planetary lander capsule surface materials
Paik, W. W.↗
Electronic packaging and cabling of a Mars rough lander
Electronic packaging and cabling on Capsule System Advanced Development Lander for Mars rough landing
Read, W. S.↗
Effect of trajectory, guidance, and environmental parameters and uncertainties on the design optimization of the out-of-orbit Viking soft lander
Trajectory, guidance and environmental parameters and uncertainties effect on design optimization of out-of-orbit Viking soft lander
Mukhopadhyay, A. K.↗
Orbit and position determination for Mars orbiters and landers
Statistical orbit and position determination for Mars orbiters and landers based on Viking 1973 mission requirements, discussing tracking problems
Anderson, S. G.↗
Martian soft lander insulation study
Insulation materials selection for Martian soft lander to meet mission environmental conditions based on tests
Conti, J. C.↗
Subsystem weight trade-off studies for the design optimization of an out-of-orbit Mars soft lander
Subsystem weight trade-offs for design optimization of out-of-orbit Mars soft lander, using atmosphere and surface environmental Monte Carlo model
Mukhopadhyay, A. K.↗
Manned Mars lander launch-to-rendezvous analysis for a 1981 Venus-swingby mission
Manned Mars lander launch-to-rendezvous analysis, using subsequent Venus swingby for mission velocity requirement reduction
Faust, N. L.↗
The Viking Mars Lander decelerator system
Parachute decelerator system for 1975 Viking Mars Lander mission, discussing configuration selection, design factors, trajectory simulation, weight and mass analysis, etc
Hussong, J. C.↗
Orbit and position determination for Mars orbiters and landers
Statistical orbit and position determination for Mars orbiters and landers based on Viking 1973 mission requirements, discussing tracking problems
Anderson, S. G.↗
A preliminary analysis of the radiation burden of a typical Mars lander mission
Predicted radiation dosage for Mars lander mission
Dugan, V. L.↗
Longitudinal aerodynamic characteristics of the Viking lander capsule at Mach 6
Longitudinal aerodynamic characteristics of Viking lander spacecraft at hypersonic speed
Emery, J. C.↗
Experience applicable to the Viking lander from a study of related space flight projects
Related space mission data for baseline evaluation of Viking Lander design and operation
Butterfield, A. J.↗
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.↗
Mars lander deorbit trajectory analysis
Mars lander deorbit trajectory sensitivity analysis for fixed flight path and communications angles at atmospheric entry, comparing with Monte Carlo simulation
Euler, E. A.↗
A technique for lifting entry and terminal phase system optimization for the 1975 Mars Viking lander
Lifting entry and terminal phase system optimization for 1975 Mars Viking lander, considering graphical tradeoff approach including design parameter and atmosphere model variations
French, C. E.↗