Synthesis of an evolutionary lunar exploration plan.
Lunar exploration planning methodology for after post-Apollo landing based on equipment evolution
MANNED SPACE FLIGHT↗
Engineering topics
Shapland, D. J.
Publications and source records attributed to Shapland, D. J..
A comparative design analysis of three configurational families for manned earth entry at hyperbolic speeds.
Optimum entry vehicle design using aerobreaking for manned earth entry at hyperbolic speeds, examining blunted conic, biconic and tetrahedral configurations
SPACECRAFT DESIGN↗
A comparative design analysis of three configurational families for manned earth entry at hyperbolic speeds.
Optimum entry vehicle design using aerobreaking for manned Earth entry at hyperbolic speeds, examining blunted conic, biconic and tetrahedral configurations
ATMOSPHERIC ENTRY↗
A configuration for re-entry from mars missions using aerobraking.
Reentry vehicle configuration from manned Mars missions, using aerobraking
REENTRY VEHICLE↗
Asteroid belt and jupiter flyby mission study final report
Asteroid belt and Jupiter flyby mission study
INTERPLANETARY FLIGHT↗
Preliminary investigation of unmanned missions to the asteroid belt with growth potential for a Jupiter flyby.
Asteroid belt flyby spacecraft concepts based on Atlas family with potential growth for Jupiter flyby
JUPITER /PLANET/↗
Preliminary design of a mars-mission earth reentry module
Earth reentry vehicle for use in manned mars mission
MANNED SPACE FLIGHT↗
THE DYNAMIC MODEL - AN ENGINEERING APPROACH TO THE PROBLEM OF TOLERANCE TO ABRUPT ACCELERATIONS
The dynamic model - an engineering approach to the problem of tolerance to abrupt accelerations
HUMAN PERFORMANCE↗