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Advanced technology satellite demodulator developmentFord Aerospace has developed a proof-of-concept satellite 8 phase shift keying (PSK) modulation and coding system operating in the Time Division Multiple Access (TDMA) mode at a data range of 200 Mbps using rate 5/6 forward error correction coding. The 80 Msps 8 PSK modem was developed in a mostly digital form and is amenable to an ASIC realization in the next phase of development. The codec was developed as a paper design only. The power efficiency goal was to be within 2 dB of theoretical at a bit error rate (BER) of 5x10(exp 7) while the measured implementation loss was 4.5 dB. The bandwidth efficiency goal was 2 bits/sec/Hz while the realized bandwidth efficiency was 1.8 bits/sec/Hz. The burst format used a preamble of only 40 8 PSK symbol times including 32 symbols of all zeros and an eight symbol unique word. The modem and associated special test equipment (STE) were fabricated mostly on a specially designed stitch-weld board although a few of the highest rate circuits were built on printed circuit cards. All the digital circuits were ECL to support the clock rates of from 80 MHz to 360 MHz. The transmitter and receiver matched filters were square-root Nyquist bandpass filters realized at the 3.37 GHz i.f. The modem operated as a coherent system although no analog phase locked (PLL) loop was employed. Within the budgetary constraints of the program, the approach to the demodulator has been proven and is eligible to proceed to the next phase of development of a satellite demodulator engineering model. This would entail the development of an ASIC version of the digital portion of the demodulator, and MMIC version of the quadrature detector, and SAW Nyquist filters to realize the bandwidth efficiency.
Document ID
19910001821
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ames, Stephen A.
(Ford Aerospace Corp. Palo Alto, CA, United States)
Date Acquired
September 6, 2013
Publication Date
August 29, 1989
Subject Category
Communications And Radar
Report/Patent Number
NAS 1.26:185127
NASA-CR-185127
Report Number: NAS 1.26:185127
Report Number: NASA-CR-185127
Accession Number
91N11134
Funding Number(s)
CONTRACT_GRANT: NAS3-24678
PROJECT: RTOP 650-60-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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