The effects of tracking station location uncertainty and measurement bias errors during phases of the Apollo mission
Effects of measurement noise, measurement bias, and station location uncertainties on Apollo mission phases
NAVIGATION SYSTEM↗
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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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Effects of two probe antennas on aerodynamic characteristics of Apollo spacecraft at Mach 10.03
Effects of two interchangeable probe antennas on aerodynamic characteristics of Apollo reentry vehicle model at Mach number 10.03
ANTENNA↗
Aerodynamic stability characteristics of the Apollo launch escape vehicle
Aerodynamic stability of Apollo launch escape vehicle
LAUNCH ESCAPE SYSTEM /LES/↗
A Feasibility Study on Miniaturizing an Automatic Amino Acid Analyzer for Use on Apollo Mission and Mars Voyager Mission Progress Report, Jan. - Jun. 1967
Miniaturizing n automatic amino acid analyzer for use on Apollo mission and Mars Voyager mission
AMINO ACID↗
Microcircuit applications in the Apollo TV CAMERA
Microcircuit design concepts applicable to Apollo television camera
MICROCIRCUIT↗
Low-speed dynamic model investigation of Apollo command module configurations in the Langley spin tunnel
Dynamic stability of Apollo command module with and without drogue parachutes at low subsonic speeds in spin tunnel
COMMAND MODULE↗
Calculation of signal margins for the CSM UNIFIED S-band downlink channel Apollo AS-202 to aircraft NASA 432
Signal margin calculation procedures for CSM UNIFIED S-BAND downlink channel Apollo AS-202 TO aircraft NASA 432
SIGNAL TRANSMISSION↗
Qualification evaluation of the pitch control motor for the launch escape system of the Apollo spacecraft program
Environmental testing and static firing of pitch control motor for Apollo spacecraft launch escape system
ESCAPE ROCKET↗
The feasibility of a direct relay of Apollo spacecraft data via a communication satellite
Feasibility of direct relay of Apollo spacecraft data via communications satellite
APOLLO SPACECRAFT↗
Dynamic model investigation of water pressures and accelerations encountered during landings of the Apollo spacecraft
Apollo spacecraft landing simulation to determine impact water pressures, accelerations, and landing dynamics
SPACECRAFT LANDING↗
Entry flight aerodynamics from Apollo mission AS-202
Entry flight aerodynamics from Apollo mission AS-202
AERODYNAMIC CHARACTERISTICS↗
Analysis of crew performance in the Apollo command module, phase I. Volume II - Appendix
Analysis of crew performance in Apollo command module
ASTRONAUT PERFORMANCE↗
Analysis of crew performance in the Apollo command module, phase I
Crew performance in Apollo command module during 7-day lunar landing simulations
COMMAND MODULE↗
An integrated NASA tracking network for Apollo
Integrated NASA tracking antenna network for Apollo missions using spacecraft transponder
TRACKING ANTENNA↗
Station contact times for Apollo orbits with variable launch azimuths
Graphs of station contact times for Apollo parking orbits with variable launch azimuths
PARKING ORBIT↗
Command angle torquing of gyros in the Apollo Guidance and Navigation System.
Apollo Guidance and Navigation System positioning by electrically torquing gyros, discussing error sources
NAVIGATION AND GUIDANCE↗
The Apollo launch data telemetry system.
The development of the Apollo Launch Data Telemetry System, the real-time interface between the Merritt Island Launch Area (MILA) and the Mission Control Center-Houston (MCC-H), is reviewed from its beginning through the system planning stages, and then into the final hardware implementation.
REAL TIME↗
The Apollo X-ray astronomy experiment.
Apollo X-ray astronomy experiment, noting instrumentation techniques employed and advantages
X-RAY ASTRONOMY↗