Digital communication and tracking - Ranging subsystem acquisition probabilities
Error acquisition probability in Mark 1 ranging subsystem as function of signal-to-noise ratio and integration time used in correlation
CORRELATION FUNCTION↗
SEARCH · Search NASA
Results for “Subsystem”
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
S-band Receiver-Exciter Ranging subsystem /RER/, Blocks IIB and IIIC
S-band receiver exciter ranging subsystem Blocks IIB and IIIB
RADAR RECEIVER↗
Conference nets of the operational voice communications subsystems
Conference nets of operational voice communications subsystem
VOICE COMMUNICATION↗
Ranger TV subsystem flight evaluation report for flight model III-3 /RA-8/
Performance evaluation of Ranger VIII Flight Model III-3 television subsystem
TELEVISION EQUIPMENT↗
Vent subsystem - development plan
Vent subsystem design specifications for use in fuel cell assembly
EQUIPMENT SPECIFICATIONS↗
Nimbus-B solar conversion power supply subsystem Quarterly technical report, Dec. 1966 - Feb. 1967
Nimbus-B solar conversion power supply subsystem
SOLAR CONVERTER↗
Conceptual mechanization studies for a horizon definition spacecraft electrical power subsystem
Solar cell-battery electrical power subsystem for horizon definition spacecraft
SOLAR CELL↗
Conceptual mechanization studies for a horizon definition spacecraft structures and thermal subsystem
Conceptual mechanization for horizon definition spacecraft structures and thermal subsystem - spin-stabilized, hexagonal cylinder for launch of two-stage Improved Delta /DSV-3N/
SPACECRAFT CONFIGURATION↗
Conceptual mechanization studies for a horizon definition spacecraft attitude control subsystem, phase A, part II, 10 October 1966 - 29 May 1967
Attitude control subsystem for spin stabilized spacecraft for mapping earths infrared horizon radiance profiles in 15 micron carbon dioxide absorption band
SPIN STABILIZATION↗
Development of visual, contact and decision subsystems for a Mars rover, July 1966 - January 1967
Visual, contact, and decision subsystems for Mars rover
DECISION MAKING↗
Research and advanced development. Volume III - Supporting research and technology for the office of tracking and data acquisition /new systems and spacecraft subsystems/, National Aeronautics and Space Administration Semiannual review, 1 Jan. - 30
Tracking and data acquisition supporting research and technology /new systems and spacecraft subsystems/
SPACECRAFT TRACKING↗
Voyager capsule phase B. Volume III - Surface laboratory system. Part C1 - Subsystem functional description Final report
Voyager capsule surface laboratory system - subsystem functional descriptions
SPACE CAPSULE↗
Voyager capsule phase B. Volume III - Surface laboratory system. Part C2 - Subsystem functional description Final report
Voyager capsule surface laboratory system - subsystem functional descriptions
SPACE CAPSULE↗
Definition of science subsystems for Jupiter flyby missions.
Science subsystems for Jupiter flyby missions, discussing equipment selection, mission planning, spacecraft design and trajectory and constraints on vehicle configuration
PLANETARY EXPLORATION↗
Optical technical Apollo extension system, phase A, volume 5. Section 5 - Subsystem design Final technical report
Optical communication equipment design and integration - propulsion subsystem - guidance, navigation, and environmental control
Source record↗
Magnetic field restraints for spacecraft systems and subsystems
Techniques for limiting magnetic fields generated by spacecraft systems and subsystems
Harris, C. A.↗
Image dissector camera subsystem, associated ground support equipment, and integration support for applications technology satellite Quarterly report, Nov. 17, 1966 - Feb. 17, 1967
Image dissector camera subsystem fabrication and ground support equipment development for ATS
Source record↗
Voyager spacecraft phase B, task D. Volume 2 - System description. Book 3 - Guidance and control, computer and sequencer, power subsystem, electrical system Final report
Baseline design and functional requirements of Voyager spacecraft guidance and control, computer and sequencer, and power subsystems, and electrical system
Source record↗