The NASA spacecraft transponding modem
A new deep space transponder is being developed by the Jet Propulsion Laboratory for NASA. The spacecraft transponding modem (STM) implements standard transponder functions and some of the command and telemetry channel service functions that have resided in spacecraft Command/Data Subsystems. The ST...
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description | A new deep space transponder is being developed by the Jet Propulsion Laboratory for NASA. The spacecraft transponding modem (STM) implements standard transponder functions and some of the command and telemetry channel service functions that have resided in spacecraft Command/Data Subsystems. The STM tracks an X-band uplink signal and provides both X-band and Ka-band downlinks, either coherent or noncoherent with the uplink. A command detector is integrated into the STM, along with a codeblock processor and a hardware command decoder. The STM provides Reed-Solomon coding, convolutional coding, and turbo coding for downlink telemetry. The downlink symbol rates can be linearly ramped to match the G/T curve of the receiving station. Data rates range from 5 bits per second (bps) to 24 Mbps, with three modulation modes provided: subcarrier, biphase-L direct on carrier, and offset-QPSK. Standard turn around ranging, regenerative pseudo-noise ranging capability, and Differential One-way Ranging (DOR) tones are provided. |
doi_str_mv | 10.1109/AERO.2000.879288 |
format | Conference Proceeding |
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The spacecraft transponding modem (STM) implements standard transponder functions and some of the command and telemetry channel service functions that have resided in spacecraft Command/Data Subsystems. The STM tracks an X-band uplink signal and provides both X-band and Ka-band downlinks, either coherent or noncoherent with the uplink. A command detector is integrated into the STM, along with a codeblock processor and a hardware command decoder. The STM provides Reed-Solomon coding, convolutional coding, and turbo coding for downlink telemetry. The downlink symbol rates can be linearly ramped to match the G/T curve of the receiving station. Data rates range from 5 bits per second (bps) to 24 Mbps, with three modulation modes provided: subcarrier, biphase-L direct on carrier, and offset-QPSK. 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The spacecraft transponding modem (STM) implements standard transponder functions and some of the command and telemetry channel service functions that have resided in spacecraft Command/Data Subsystems. The STM tracks an X-band uplink signal and provides both X-band and Ka-band downlinks, either coherent or noncoherent with the uplink. A command detector is integrated into the STM, along with a codeblock processor and a hardware command decoder. The STM provides Reed-Solomon coding, convolutional coding, and turbo coding for downlink telemetry. The downlink symbol rates can be linearly ramped to match the G/T curve of the receiving station. Data rates range from 5 bits per second (bps) to 24 Mbps, with three modulation modes provided: subcarrier, biphase-L direct on carrier, and offset-QPSK. Standard turn around ranging, regenerative pseudo-noise ranging capability, and Differential One-way Ranging (DOR) tones are provided.</description><subject>Detectors</subject><subject>Downlink</subject><subject>Hardware</subject><subject>Laboratories</subject><subject>Modems</subject><subject>NASA</subject><subject>Propulsion</subject><subject>Space vehicles</subject><subject>Telemetry</subject><subject>Transponders</subject><issn>1095-323X</issn><issn>2996-2358</issn><isbn>9780780358461</isbn><isbn>0780358465</isbn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2000</creationdate><recordtype>conference_proceeding</recordtype><sourceid>6IE</sourceid><sourceid>RIE</sourceid><recordid>eNotj0tLw0AUhQcfYFq7F1dZuZs4j2TmzjKUVoXSglZwV-7M3GrEpCGTjf_eQIUDh29xPjiM3UlRSCncY7163RVKCFGAdQrggmXKOcOVruCSLZwFMWWC0sgrlk2TimulP27YLKVvIZRQIDL2sP-ifFu_1XnqMVAY8Djm44Bd6k9dbLrPvD1Fam_Z9RF_Ei3-e87e16v98plvdk8vy3rDG2nVyCMGqIzHUEmgoL0lL8EaTTLYGEMFymlJuiTrDaJ2GJ03BOgCKlMaq-fs_uxtiOjQD02Lw-_h_FD_Af77Qdo</recordid><startdate>2000</startdate><enddate>2000</enddate><creator>Berner, J.B.</creator><creator>Kayalar, S.</creator><creator>Perret, J.D.</creator><general>IEEE</general><scope>6IE</scope><scope>6IH</scope><scope>CBEJK</scope><scope>RIE</scope><scope>RIO</scope></search><sort><creationdate>2000</creationdate><title>The NASA spacecraft transponding modem</title><author>Berner, J.B. ; Kayalar, S. ; Perret, J.D.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-i172t-dac856bac518ec3b7eb18763e1c7ddc582931e34e7b6aa39ad9b6e8a9ca264673</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2000</creationdate><topic>Detectors</topic><topic>Downlink</topic><topic>Hardware</topic><topic>Laboratories</topic><topic>Modems</topic><topic>NASA</topic><topic>Propulsion</topic><topic>Space vehicles</topic><topic>Telemetry</topic><topic>Transponders</topic><toplevel>online_resources</toplevel><creatorcontrib>Berner, J.B.</creatorcontrib><creatorcontrib>Kayalar, S.</creatorcontrib><creatorcontrib>Perret, J.D.</creatorcontrib><collection>IEEE Electronic Library (IEL) Conference Proceedings</collection><collection>IEEE Proceedings Order Plan (POP) 1998-present by volume</collection><collection>IEEE Xplore All Conference Proceedings</collection><collection>IEEE Electronic Library (IEL)</collection><collection>IEEE Proceedings Order Plans (POP) 1998-present</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Berner, J.B.</au><au>Kayalar, S.</au><au>Perret, J.D.</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>The NASA spacecraft transponding modem</atitle><btitle>2000 IEEE Aerospace Conference. Proceedings (Cat. No.00TH8484)</btitle><stitle>AERO</stitle><date>2000</date><risdate>2000</risdate><volume>7</volume><spage>195</spage><epage>209 vol.7</epage><pages>195-209 vol.7</pages><issn>1095-323X</issn><eissn>2996-2358</eissn><isbn>9780780358461</isbn><isbn>0780358465</isbn><abstract>A new deep space transponder is being developed by the Jet Propulsion Laboratory for NASA. The spacecraft transponding modem (STM) implements standard transponder functions and some of the command and telemetry channel service functions that have resided in spacecraft Command/Data Subsystems. The STM tracks an X-band uplink signal and provides both X-band and Ka-band downlinks, either coherent or noncoherent with the uplink. A command detector is integrated into the STM, along with a codeblock processor and a hardware command decoder. The STM provides Reed-Solomon coding, convolutional coding, and turbo coding for downlink telemetry. The downlink symbol rates can be linearly ramped to match the G/T curve of the receiving station. Data rates range from 5 bits per second (bps) to 24 Mbps, with three modulation modes provided: subcarrier, biphase-L direct on carrier, and offset-QPSK. Standard turn around ranging, regenerative pseudo-noise ranging capability, and Differential One-way Ranging (DOR) tones are provided.</abstract><pub>IEEE</pub><doi>10.1109/AERO.2000.879288</doi></addata></record> |
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language | eng |
recordid | cdi_ieee_primary_879288 |
source | IEEE Electronic Library (IEL) Conference Proceedings |
subjects | Detectors Downlink Hardware Laboratories Modems NASA Propulsion Space vehicles Telemetry Transponders |
title | The NASA spacecraft transponding modem |
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