Terminal descent simulation study Final report
Simulation program for parachute and terminal descent phases of Mars soft lander
Broderick, R. F.↗
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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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Capsule system advanced development sterilization program
Capsule system advanced development sterilization program for Mars 71 lander
Christensen, M. R.↗
Mission constraints on solid-propellant motors for unmanned spacecraft.
Mission and planetary vehicles characteristics affecting design of solid propellant motors and thrust vector control systems in planetary orbiters and landers
Cork, M. J.↗
Effects of simulated Mars dust erosion environment on thermal control coatings.
Thermal control coatings, windows and mirrors for 1973 Mars Viking Lander vehicles under simulated Martian surface conditions
Adlon, G. L.↗
Exobiology and the exploration of Mars.
Mars exploration for life by Mariner flybys and orbiters and 1973 Viking landers
Rea, D. G.↗
Solar array configurations and performance on the Martian surface.
Solar array configurations and performance on Martian surface, including hard lander design and surviving shock levels
Hasbach, A.↗
Jettisoning system for a parachute's canister
Three-point automatically released suspension and jettisoning system operates independently of lander's power system and releases parachute on touchdown. The system is based on a ball-lock device operated by the shock of the parachute's opening and by the subsequent decay in the load on the main cord.
Lonborg, J. O.↗
Long range planning for solar system exploration Quarterly report, 1 May - 1 Aug. 1969
Spacecraft radar systems and Jupiter Moon lander mission planning
Source record↗
Demonstration of a sterilizable solid propellant rocket motor Final report, Feb. 1969 - Jul. 1970
Demonstration of solid propellant rocket engine for unmanned planetary landers to withstand dry heat sterilization
Weinberg, L.↗
Multispectral discrimination of possible Martian surface constituents
Multispectral imaging from lander for Martian surface constituents discrimination
Klemas, V.↗
An analysis and simulation of Mars landing
Mars landing analysis and simulation for unmanned lander prototype, discussing digital simulation by Monte Carlo techniques and physical tests
Casani, E. K.↗
Subsystem weight trade-off studies for the design optimization of a planetary landing vehicle
Computerized tradeoff analysis for planetary landing vehicle entry capsule and lander design optimization, emphasizing weight allocation for Mars 1973 missions
Mukhopadhyay, A. K.↗
Discrimination of possible Martian surface constituents by multispectral imaging
Martian multispectral imaging from lander emphasizing spectral bands and gray levels number for discrimination of surface constituents
Klemas, V.↗
Effects of Simulated Mars Dust Erosion Environment on Thermal Control Coatings
Thermal control coatings, windows and mirrors for 1973 Mars Viking Lander vehicles under simulated Martian surface conditions
Adlon, G. L.↗
Navigational approaches to planetary orbiters and rovers
Navigation for planetary orbiter and lander missions, considering orbit insertion, trim corrections and capsule descent for poor planetary gravity field model
Moore, J. W.↗
Monte Carlo modeling of the Martian atmosphere from Viking mission design point of view
Martian atmosphere modeling for obtaining Viking lander spacecraft design margins by Monte Carlo method
Mukhopadhyay, A. K.↗
Unmanned exploration of Mars
Mariner, Explorer, High Data Orbiters, Viking and Rover landers as required systems for unmanned Mars exploration, examining ballistic and lifting entry
Harrison, E. F.↗
A parameter dependent spacecraft guidance boundary value problem
Spacecraft trajectory initial conditions expressions as parameters dependent functions, applying results to Mars lander mission
Cefola, P. J.↗
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