Apollo mission description
This paper describes a typical Apollo lunar landing mission. The particular example chosen provides a 24-hour stay on the lunar surface and has a total duration of slightly more than eight days.
LANDING SITE↗
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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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Spacecraft description
Command, service, and excursion modules of lunar exploration spacecraft, and communication links with earth stations
SERVICE MODULE↗
Hydrodynamic description of a strongly- rarefied plasma
Hydrodynamic equations to describe collisionless plasma
MOTION EQUATION↗
Princeton advanced satellite study. Volume III - 40-inch system description
Optical design and characteristic parameters of 40-inch large aperture telescope package for orbiting astronomical satellite
SCIENTIFIC SATELLITE↗
Description of the Computerized Reliability Analysis Method /CRAM/ Arinc Research monograph no 11
Computer Reliability Analysis Method /CRAM/ TO analyze reliability by using utility routines
COMPUTER METHOD↗
Synoptic description of the 5577 angstrom nightglow near 78 deg west longitude
Diurnal and latitude variations in zenith nightglow intensity
INTENSITY↗
Description and status of DOD Gemini experiment D-12 Astronaut Maneuvering Unit /AMU/.
DOD Gemini experiment D-12 astronaut maneuvering unit /AMU/ design, detailing propulsion, flight control, oxygen and power supply, abort-alarm and communications
EXTRAVEHICULAR OPERATION↗
Description of film - Cavitation bubble dynamics in water and liquid mercury.
Behavior of individual cavitation bubbles in cavitating flows of water and liquid Mercury, using two-dimensional Plexiglas venturi
FLOW VISUALIZATION↗
Description of film - Cavitation hysteresis.
Motion picture on cavitation hysteresis, details on test apparatus, noting cavitation delay time
CAVITATION FLOW↗
Description of film - Cavitation in a mixed- flow pump.
Cavitation performance testing in water of mixed flow pump impeller
CAVITATION FLOW↗
Description of a new parachute designed for use with meteorological rockets and a consideration of improvements in meteorological measurements.
Parachute for meteorological rockets, noting design, testing, high altitude performance, etc
PARACHUTE FABRIC↗
Synoptic description of the 6300 angstrom units nightglow near 78 deg West longitude.
Diurnal and latitudinal variations in 6300 angstrom nightglow intensity determined along Pacific coast of South America, noting relation between location of antisolar point and equatorial midnight enhancement
OXYGEN SPECTRUM↗
Nonlinear mechanical model for the description of propellant sloshing.
Planar and rotary sloshing motion of liquid, using analytic mechanical model that consists of mass point constraint to parabolic surface
PROPELLANT STORAGE↗
Description and status of the Saturn IB PROGRAM.
Trajectory and performance analysis instrument unit and payload envelope for Saturn IB space vehicle program
SPACECRAFT DESIGN↗
A set of parameters for the description of orbits of space vehicles sistema parametrov dlya opisaniya orbit kosmicheskikh apparatov
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Samoylovich, G. V.↗
Mariner iv measurements near mars - initial results. spacecraft description and encounter sequence
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Anderson, H. R.↗
Inviscid analysis of the plume created by multiple rocket engines. Part II - Description of the computer programs
Computer program for calculation of single jet and five jet interaction regimes associated with multiple rocket engines
ROCKET ENGINE↗
Description of the installations at the Pleumeur-Bodou Space Communications Station
The Pleumeur-Bodou Ground Station, the research center of the National Ceneter for Telecommunications, is equipped to study all problems connected with active satellites: link performance, acquisition, tracking, telemetry, and command. This station is also intended for possible future commercial applications.
COMMUNICATIONS SATELLITE↗