TY - JOUR
T1 - VLF wave experiments in space using a modulated electron beam
AU - John Raitt, W.
AU - Emstmeyer, James
AU - Myers, Neil B.
AU - White, A. Brent
AU - Sasaki, Susumu
AU - Oyama, Koh Ichiro
AU - Kawashima, Nobuki
AU - Fraser-Smith, Anthony C.
AU - Gilchrist, Brian E.
AU - Hallinan, Thomas J.
N1 - Funding Information:
This project was supported by NASA Grants NAG5-607, NAG5-658, and NAGW 1817 to Utah State University and by Rome Laboratory Contracts Fl9628-9l-K-0037 to USU, F19628-89-K-0040 to Stanford University, and Fl9628-9l-K-0035 to the University of Alaska. We would like to thank the many engineers and tech- nicians at USU/SDL, ISAS, Rome Laboratory, Wallops Flight Facility, and PFRR, all of whom contributed to make the mission a success. In particular we thank David Kotsifakis of WFF and Ron Pierce of PFRR, who managed the NASA operations at the inte- gration facility and the range. Several theorists helped to define the frequencies and ground locations of the vlf receivers, and we would like to acknowledge in particular the assistance of Peter M. Banks, Ken Marker, and Torsten Neubert. We are grateful to Donald C. Thompson for adapting his general-purpose data-handling and graphicsprograms to speed upthedata reduction.Wewould also like to recognize the vision of the late Stanley Shawhan of NASA Headquarters, who recognized the value of the space environment as a place to perform unique physics experiments, and the practicality of combining NASA resources with those of other agencies to accom- plish projects that would otherwise have languished through lack of funding.
PY - 1995
Y1 - 1995
N2 - A sounding-rocket payload to study the generation and emission of electromagnetic waves from a modulated electron beam was developed and successfully flown from the Poker Flat Research Range, Alaska, in March 1992 on a Black Brant 11 sounding rocket. We describe the mission objectives, the instrumentation, flight operations, and preliminary results from the flight. The payload contained a modulated electron gun with a triode arrangement of electrodes allowing modulation of the beam current up to vlf frequencies. Vehicle charging was inhibited by a gas-release system, synchronized with the beam emissions. A network of ground stations was set up to try to receive signals from the modulated beam, and low-light systems were set up to look for evidence of the beam below the payload trajectory. No evidence of beam-induced wave radiation to the ground was detected. However, strong vlf frequencies following the preset program were clearly detected by the diagnostic free flyer and the tethered daughter payload segment. The effect of the gas releases was very marked. The vehicle potential dropped from over 1 kV to about 30 V when the gas was turned on. Some evidence of the light from beam-atmosphere interactions was seen near the end of the flight, but in general, the optical results were not very informative. The launch was successful, mission operations were as planned, and good-quality onboard data were collected throughout the operational part of the flight.
AB - A sounding-rocket payload to study the generation and emission of electromagnetic waves from a modulated electron beam was developed and successfully flown from the Poker Flat Research Range, Alaska, in March 1992 on a Black Brant 11 sounding rocket. We describe the mission objectives, the instrumentation, flight operations, and preliminary results from the flight. The payload contained a modulated electron gun with a triode arrangement of electrodes allowing modulation of the beam current up to vlf frequencies. Vehicle charging was inhibited by a gas-release system, synchronized with the beam emissions. A network of ground stations was set up to try to receive signals from the modulated beam, and low-light systems were set up to look for evidence of the beam below the payload trajectory. No evidence of beam-induced wave radiation to the ground was detected. However, strong vlf frequencies following the preset program were clearly detected by the diagnostic free flyer and the tethered daughter payload segment. The effect of the gas releases was very marked. The vehicle potential dropped from over 1 kV to about 30 V when the gas was turned on. Some evidence of the light from beam-atmosphere interactions was seen near the end of the flight, but in general, the optical results were not very informative. The launch was successful, mission operations were as planned, and good-quality onboard data were collected throughout the operational part of the flight.
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U2 - 10.2514/3.55687
DO - 10.2514/3.55687
M3 - Article
AN - SCOPUS:0029343316
SN - 0022-4650
VL - 32
SP - 670
EP - 679
JO - Journal of Spacecraft and Rockets
JF - Journal of Spacecraft and Rockets
IS - 4
ER -