DocumentCode :
3047626
Title :
Rendezvous radar for the orbital maneuvering vehicle
Author :
Locke, John ; Olds, Keith ; Ohe, Thomas
Author_Institution :
Motorola Inc., Chandler, AZ, USA
fYear :
1990
fDate :
7-10 May 1990
Firstpage :
38
Lastpage :
43
Abstract :
The rendezvous radar set (RRS) under development will be a key subsystem aboard NASA´s new orbital maneuvering vehicle (OMV). The RRS is an X-band all solid-state, monopulse tracking, frequency-hopping, pulse-Doppler radar system. Targets of 1 m2 are detected at ranges greater than 4.5 nautical miles, and larger targets are detected at up to 10 nautical miles. The target is then tracked in angle, range, and range rate to a distance of 35 feet from the OMV. In addition to performance and cost, the design drivers for the RRS development have included the minimization of power consumption, size, and weight
Keywords :
frequency agility; radar systems; space vehicles; NASA; X-band; frequency-hopping; monopulse tracking; orbital maneuvering vehicle; pulse-Doppler radar; rendezvous radar; solid-state; target tracking; Costs; Doppler radar; Energy consumption; Frequency; Meteorological radar; Radar detection; Radar tracking; Solid state circuits; Target tracking; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Radar Conference, 1990., Record of the IEEE 1990 International
Conference_Location :
Arlington, VA
Type :
conf
DOI :
10.1109/RADAR.1990.201134
Filename :
201134
Link To Document :
بازگشت