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LAUNCH VEHICLE EXHAUST PLASMA / PLUME EFFECTS ON GROUND TELEMETRY RECEPTION, STARS FT-04-1McWhorter, Mark 10 1900 (has links)
ITC/USA 2006 Conference Proceedings / The Forty-Second Annual International Telemetering Conference and Technical Exhibition / October 23-26, 2006 / Town and Country Resort & Convention Center, San Diego, California / This paper discusses the effect of vehicle exhaust plasma/plume on the ability to receive telemetered data via an S-band RF link. The data presented herein were captured during the launch of the STARS FT-04-1 on February 23, 2006 from Kodiak Launch Center, Kodiak, Alaska using Alaska Aerospace Development Corporation’s (AADC) Range Safety and Telemetry System (RSTS), designed and integrated by Honeywell.
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LAUNCH VEHICLE EXHAUST PLASMA / PLUME EFFECTS ON GROUND TELEMETRY RECEPTION, STARS IFT-14McWhorter, Mark 10 1900 (has links)
ITC/USA 2005 Conference Proceedings / The Forty-First Annual International Telemetering Conference and Technical Exhibition / October 24-27, 2005 / Riviera Hotel & Convention Center, Las Vegas, Nevada / This paper discusses the effect of vehicle exhaust plasma/plume on the ability to receive telemetered
data via an S-band RF link. The data discussed herein was captured during the launch of the STARS
IFT-14 on February 13, 2005 from Kodiak Launch Center, Kodiak, Alaska using Alaska Aerospace
Development Corporation’s (AADC) Range Safety and Telemetry System (RSTS), designed and
integrated by Honeywell.
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ROCKET MOTOR PLUME EFFECTS ON TM SIGNALS - MODEL CORROBORATIONJohnston, Jerry W., LaPoint, Steve 10 1900 (has links)
International Telemetering Conference Proceedings / October 28-31, 1996 / Town and Country Hotel and Convention Center, San Diego, California / This paper presents the interim results of an effort to corroborate analytic model
predictions of the effects of rocket motor plume on telemetry signal RF propagation. When
space is available, telemetry receiving stations are purposely positioned to be outside the
region of a rocket motor's plume interaction with the RF path; therefore, little historical
data has been available to corroborate model predictions for specific rocket motor types
and altitudes. RF signal strength data was collected during the flight of HERA target
missile by White Sands Missile Range (WSMR) using a transportable telemetry receiving
site specifically positioned to be within the rocket plume region of influence at
intermediate altitudes. The collected data was analyzed and compared to an RF plume
attenuation model developed for pre-mission predictions. This work was directed by the
US Army Kwajalein Atoll (USAKA)/ Kwajalein Missile Range (KMR) Safety Division.
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LAUNCH VEHICLE EXHAUST PLASMA / PLUME EFFECTS ON GROUND TELEMETRY RECEPTION, QRLV-2McWhorter, Mark 10 1900 (has links)
International Telemetering Conference Proceedings / October 21, 2002 / Town & Country Hotel and Conference Center, San Diego, California / This paper discusses the effect of vehicle exhaust plasma/plume on the ability to receive telemetered
data via an S-band RF link. The data discussed herein was captured during the launch of the QRLV-2 (Quick Reaction Launch Vehicle) on April 24, 2002 from Kodiak Launch Center, Kodiak, Alaska
using Honeywell’s BMRST (Ballistic Missile Range Safety Technology) system.
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