Color changes and absorption-line variations over the inner disk of M31 and the central regions of M32 and NGC 4472
Color changes and absorption line variations in M31, M32 and NGC 4472, attempting synthesis of M31 disk population
Gunn, J. E.↗
Engineering topics
Young, J. W.
Publications and source records attributed to Young, J. W..
Weight, volume, and center of mass of segments of the human body
Weight, volume, and center of mass of segments of human body
Clauser, C. E.↗
Analysis of Gravity Assisted Trajectories for Solar-probe and Deep-space Missions
Gravity assisted trajectories for solar probe and deep space flyby missions
Young, J. W.↗
Gemini status report.
Missions of Gemini VI through XI covering rendezvous, docking, thermal overloading, translation maneuver, etc
GEMINI PROJECT↗
Factors affecting food development for space flight.
Food packaging and handling under zero-g conditions of space
WEIGHTLESSNESS↗
Fixed-Base Simulator Studies of the Ability of the Human Pilot to Provide Energy Management Along Abort and Deep-Space Entry Trajectories
A simulation study has been made to determine a pilot's ability to control a low L/D vehicle to a desired point on the earth with initial conditions ranging from parabolic orbits to abort conditions along the boost phase of a deep-space mission. The program was conducted to develop procedures which would allow the pilot to perform the energy management functions required while avoiding the high deceleration or skipout region and to determine the information display required to aid the pilot in flying these procedures. The abort conditions studied extend from a region of relatively high flight-path angles at suborbital velocities while leaving the atmosphere to a region between orbital and near-escape velocity outside the atmosphere. The conditions studied included guidance from suborbital and superorbital aborts as well as guidance following return from a deepspace mission. In this paper, the role of the human pilot?s ability to combine safe return abort procedures with guidance procedures has been investigated. The range capability from various abort and entry conditions is also presented.
PILOT↗