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TDRSS COMPATIBLE TELEMETRY TRANSMITTERRupp, Greg 10 1900 (has links)
International Telemetering Conference Proceedings / October 28-31, 1996 / Town and Country Hotel and Convention Center, San Diego, California / An S-band telemetry transmitter has been developed for Expendable Launch Vehicles
(ELV's) that can downlink data through NASA's Tracking and Data Relay Satellite System
(TDRSS). The transmitter operates in the 2200 to 2300 MHz range and provides a number
of unique features to achieve optimum performance in the launch vehicle environment:
· Commandable QPSK or BPSK modulation format.
· Data rates up to 10 Mbps.
· Commandable concatenated coding provides superior link performance.
· Premodulation filtering produces excellent spectral containment characteristics.
· Phase noise of less than 3 degrees rms is maintained through launch and ascent
vibration profiles.
· A 30 watt nominal RF output power provides a robust RF link.
· Two RF antenna output ports with commandable selection of all power out to either
port or power split evenly between ports.
· Operating modes and conditions of the unit can be monitored through a number of
bilevel and analog outputs.
· A ruggedized mechanical design provides a reliable communications link for launch
vehicle environments.
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A Modular Approach to Hardened Subminiature Telemetry and Sensor System (HSTSS) DevelopmentCarpenter, Robert E., Schneider, Dennis 10 1900 (has links)
International Telemetering Conference Proceedings / October 25-28, 1999 / Riviera Hotel and Convention Center, Las Vegas, Nevada / In the past, typical telemetry systems for munitions and small missiles have often comprised adaptations of monolithic components originally conceived for aircraft or large missile applications. Programs have developed expensive monolithic systems to meet the needs of specific programs, but they often require extensive redesign for use by other potential users. The tri-service HSTSS Integrated Product Team (IPT) determined that a monolithic “one size fits all” approach has technical and fiscal risks. Thus, a modular approach to system development has been adopted. The HSTSS IPT is flight qualifying commercial microelectronic products designed for environments similar to that of munition interiors, and is developing microelectronic components required to complete a subminiature system. HSTSS components can then be integrated to support the form factor and measurement needs of any given user. In addition to offering a flexible system to the user, the HSTSS lends itself to upgradability (modernization through spares).
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