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- Wavesurfer 424 oscilloscope serial#
- Wavesurfer 424 oscilloscope full#
- Wavesurfer 424 oscilloscope series#
Wavesurfer 424 oscilloscope full#
The new WaveSurfer 104Xs increases the WaveSurfer Xs product line to a full 1GHz of bandwidth, with a maximum sample rate of 5GSample/sec. List price is £10,250 for the 1GHz model and £13,065 for the 2GHz model. Sampling rates for both are 5GSample/sec on four channels, interleaved to 10GSample/sec.
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Now, WaveRunner Xi has raised the bar it is available as 1GHz model (WR 104Xi) and as 2GHz model (WR 204Xi). Never before has so much performance and capability been provided in an oscilloscope with a small six inch deep footprint. In spring of 2006, WaveRunner Xi shattered the notions of what was possible in a small footprint oscilloscope. With this introduction, LeCroy is also launching the advanced Search and Analysis feature WaveScanTM as standard on all LeCroy Windows-based oscilloscopes. LeCroy‚ introduces four new oscilloscopes that expand the bandwidth of the WaveRunner Xi and WaveSurfer Xs product lines to an 2GHz bandwidth.
Wavesurfer 424 oscilloscope serial#
L., “ Magnetic Probes with Nanosecond Response Time for Plasma Experiments,” Journal of Physics E: Scientific Instruments, Vol. 5, No. 5, 1972, pp. 481–484.LeCroy launches four new models, WaveScan Search and Analysis and I2C/SPI Serial Trigger and Decode to its successful oscilloscope lines. of Mechanical and Aerospace Engineering, Princeton Univ., Princeton, NJ, 2002. E., “ Current Sheet Canting in Pulsed Electromagnetic Accelerators,” Ph.D. and Herdrich G., “ Characteristics of Plasma Properties in an Ablative Pulsed Plasma Thruster,” Physics of Plasmas, Vol. 20, No. 5, 2013, Paper 033503. and Karrer N., “ Power Train Configuration Study on a Pulsed Plasma Thruster with State-of-the-Art High Current Monitors,” 49th Joint Propulsion Conference, AIAA Paper 2013-4122, 2013. doi: JPPOEL 0748-4658 Link Google Scholar and Herdrich G., “ Propellant Utilization Efficiency in a Pulsed Plasma Thruster,” Journal of Propulsion and Power, Vol. 29, No. 6, 2013, pp. 1478–1487. doi: AIAJAH 0001-1452 Link Google Scholar and Auweter-Kurtz M., “ Investigation of the Magnetic Field in a Pulsed Plasma Thruster,” AIAA Journal, Vol. 46, No. 11, 2008, pp. 2881–2889. Nawaz A., “ Entwicklung und Charakterisierung Eines Gepulsten Instationären MPD Triebwerks Als Primärantrieb für Weltraumsonden,” Doctoral Thesis, Inst. and Hintze T., “ iMPD System Study and High Voltage Power Supply Subsystem Development at IRS,” 32nd International Electric Propulsion Conference, Electric Rocket Propulsion Society Paper 2011-150, Sept. 2011. and Auweter-Kurtz M., “ Three-Dimensional Particle-in-Cell Simulation of a Pulsed Plasma Thruster: Modelling and Challenges,” 32nd International Electric Propulsion Conference, Electric Rocket Propulsion Society Paper 2011-116, Sept. 2011.
Wavesurfer 424 oscilloscope series#
G., Physics of Electric Propulsion, McGraw–Hill Series in Missile and Space Technology, McGraw–Hill, New York, 1968, pp. 263–286. P., “ Cooperation Activities Between IRS and the University of Tokyo in the Field of Pulsed Plasma Thruster Development,” 31st International Electric Propulsion Conference, Electric Rocket Propulsion Society Paper 2009-251, 2009. and Osborn L., “ The Flight Application of a Pulsed Plasma Microthruster: The NOVA Satellite,” AIAA Paper 1982-1956, Nov. 1982. J., “ Solid Propellant Pulsed Plasma Propulsion System Development for North–South Stationkeeping,” AIAA Paper 1979-2097, 1979. J., “ Pulsed Plasma Thruster,” Journal of Propulsion and Power, Vol. 14, No. 5, 1998, pp. 716–735. The current density data are discussed and compared to high-speed camera photographs. It is concluded that no distinct movement of a current sheet was observed. Maximum current densities of 80 kA / m 2 and magnetic flux densities of up to 0.82 T have been observed close to the surface of the solid Teflon® propellant.
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Quantitative determination of the temporal behavior of vectors at 27 points evenly distributed in three planes delivers a comprehensive picture of the position and development of the current in a pulsed plasma thruster. The local magnetic field components of all three spatial directions are combined to derive the current density vector.
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This is achieved by building and calibrating miniaturized induction probes. The work presented in this paper covers new information on the electromagnetic conditions during thrust generation by revealing the temporal and spatial distributions of the current density vectors between the thruster electrodes. The pulsed plasma thruster of the magnetoplasmadynamic type represents a promising and cheap solution to today’s propulsion challenges in space.