A UNIQUE APPROACH TO AN X-BAND TELEMETRY RECEIVING SYSTEM
A unique approach to an x-band telemetry receiving system
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A unique approach to an x-band telemetry receiving system
X-band telemetering for radio interference - reentry communication in earth orbit reentry vehicle
Metal X-band waveguide cell for study of microwave propagation through magnetoplasma
X-band solid state signal source microwave apparatus
Continuous wave amplitude modulation of gallium arsenide injection lasers at X-band
Metal X-band circular waveguide cell containing discharge electrodes for study of microwave propagation in magnetoplasma
Short term frequency stability measurements of crystal controlled X-band source - spectral measurements by oscillator and harmonic generator in vibrational environment
X-band gain measurement of Venus Deep Space Instrumentation Facility antennas
Description of an x-band telemetry receiving system for communication during reentry
X-band reentry telemetry system
Theoretical and experimental evaluation of radar boresight range on Merrit Island
Central frequency synthesizer performance and voltage controlled oscillator static phase error
Geologic analysis of X band radar mosaics of Massachusetts
X-band target simulator with spectral purity for long radar echo pulses
Small frequency shift measurement method for X-band plasma-loaded cavities
Direct phase reading X-band radio interferometer for attitude control of Applications Technology Satellite-4
Topical communication in the context of a deep space communication link. Communication link analysis at the optical frequencies differs significantly from that at microwave frequencies such as the traditional S and X-bands used in deep space applications, due to the different technology of transmitter, antenna, modulators, and receivers. In addition, the important role of quantum noise in limiting system performance is quite different than that of thermal noise. The optical link design is put in a design control table format similar to a microwave telecom link design. Key considerations unique to the optical link are discussed.
The Spaceborne Imaging Radar-C/X-band Synthetic Aperture Radar (SIR-C/X-SAR) is the most advanced imaging radar system to fly in Earth orbit. Carried in the cargo bay of the Space Shuttle Endeavour in April and October of 1994, SIR-C/X-SAR simultaneously recorded SAR data at three wavelengths (L-, C-, and X-bands; 23.5, 5.8, and 3.1 cm, respectively). The SIR-C/X-SAR Science Team consists of 53 investigator teams from more than a dozen countries. Science investigations were undertaken in the fields of ecology, hydrology, ecology, and oceanography. This report contains 44 investigator team reports and several additional reports from coinvestigators and other researchers.