Summary of Gemini rendezvous experience.
Gemini rendezvous experience, describing flight test cycles, type of maneuvers needed, ground and onboard support systems, etc
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Gemini rendezvous experience, describing flight test cycles, type of maneuvers needed, ground and onboard support systems, etc
IMP-I earth satellite magnetic field measurement experimental results including solar wind flow effects
NERVA radiation effects tests at cryogenic temperatures
Economical feasibility of open and closed cycle vortex-stabilized gaseous nuclear rocket engines, investigating vortex flow characteristics
Day- and nighttime electron and ion density profiles in lower ionosphere deduced from blunt probe theory and measurements
Noncavitating water flow tests of three loaded axial flow pump rotor blades
NASA radial flow turbine research related to Brayton cycle power generator, investigating size, Reynolds number and speed effects on efficiency and flow
V/stol concepts for short haul commercial aircraft compared for gross weight, operating cost, gust sensitivity and noise levels
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Explore the source record for details and available documents.
The basic mission objective of Project Apollo is to land men on the Moon and return them to Earth at the earliest practicable date. The Apollo crew will consist of three men, two of whom will land on the surface of the Moon, conduct surface operations for up to 24 hr, and then rejoin the third crew member in lunar orbit for return to Earth. Initial Apollo spacecraft capabilities will require the early landings to be within +or-lO deg of the lunar equator on the visible side of the Moon, with preference for landing sites in the leading quadrant (between 270 and 360 deg lunar longitude). As presently planned, the Apollo spacecraft will be capable of carrying approximately 200 lb of scientific equipment to the lunar surface and of bringing approximately 80 lb of lunar material back to Earth. A detailed plan for utilization of crew capabilities while on the lunar surface is not expected to be complete for some time. The first Apollo lunar mission is now scheduled for the late 1960's with additional launches planned at reasonable intervals. i
Structure-property study of polyurethane, epoxy, polyisocyanurate, and polyoxazolidone adhesives
Probe to bus communication rates for Mars 1971 multiple probe system
Medical studies and physiological tests of Gemini 7 astronauts
Medical experiments conducted to protect Gemini astronauts from space flight stress
Recapitulation of results of lunar topography studies using radar techniques
Descriptive model for determining optimal human performance in aerospace systems
Receiver techniques and detectors for use at millimeter and submillimeter wavelengths, and excitation cross sections for argon II, krypton II, and neon II gas lasers