These tools will no longer be maintained as of December 31, 2024. Archived website can be found here. PubMed4Hh GitHub repository can be found here. Contact NLM Customer Service if you have questions.


BIOMARKERS

Molecular Biopsy of Human Tumors

- a resource for Precision Medicine *

140 related articles for article (PubMed ID: 27131673)

  • 21. Note: An advanced in situ diagnostic system for characterization of electric propulsion thrusters and ion beam sources.
    Bundesmann C; Tartz M; Scholze F; Leiter HJ; Scortecci F; Gnizdor RY; Neumann H
    Rev Sci Instrum; 2010 Apr; 81(4):046106. PubMed ID: 20441379
    [TBL] [Abstract][Full Text] [Related]  

  • 22. Evaluation of ion collection area in Faraday probes.
    Brown DL; Gallimore AD
    Rev Sci Instrum; 2010 Jun; 81(6):063504. PubMed ID: 20590238
    [TBL] [Abstract][Full Text] [Related]  

  • 23. Zeeman splitting measurements of magnetic fields in iodine plasma.
    Steinberger TE; Dufor MT; Thompson DS; Scime EE
    Rev Sci Instrum; 2018 Oct; 89(10):10C113. PubMed ID: 30399757
    [TBL] [Abstract][Full Text] [Related]  

  • 24. Measurement of axial neutral density profiles in a microwave discharge ion thruster by laser absorption spectroscopy with optical fiber probes.
    Tsukizaki R; Koizumi H; Nishiyama K; Kuninaka H
    Rev Sci Instrum; 2011 Dec; 82(12):123103. PubMed ID: 22225195
    [TBL] [Abstract][Full Text] [Related]  

  • 25. Erosion sensor using time-resolved cavity ring-down spectroscopy for Hall thrusters.
    Egawa Y; Yamamoto N; Yamaguchi A; Morita T
    Rev Sci Instrum; 2020 Nov; 91(11):113105. PubMed ID: 33261454
    [TBL] [Abstract][Full Text] [Related]  

  • 26. Improved analysis techniques for cylindrical and spherical double probes.
    Beal B; Johnson L; Brown D; Blakely J; Bromaghim D
    Rev Sci Instrum; 2012 Jul; 83(7):073506. PubMed ID: 22852694
    [TBL] [Abstract][Full Text] [Related]  

  • 27. Space Electroosmotic Thrusters in Ion Partitioning Soft Nanochannels.
    Zheng J; Jian Y
    Micromachines (Basel); 2021 Jun; 12(7):. PubMed ID: 34209246
    [TBL] [Abstract][Full Text] [Related]  

  • 28. Laser-induced fluorescence diagnostic for temperature and velocity measurements in a hydrogen arcjet plume.
    Liebeskind JG; Hanson RK; Cappelli MA
    Appl Opt; 1993 Oct; 32(30):6117-27. PubMed ID: 20856439
    [TBL] [Abstract][Full Text] [Related]  

  • 29. Calibrating ion density profile measurements in ion thruster beam plasma.
    Zhang Z; Tang H; Ren J; Zhang Z; Wang J
    Rev Sci Instrum; 2016 Nov; 87(11):113502. PubMed ID: 27910433
    [TBL] [Abstract][Full Text] [Related]  

  • 30. Design and experimental results of a laser-ignited solid-propellant-fed magnetoplasmadynamic thruster.
    Ou Y; Wu J; Zhang Y
    Rev Sci Instrum; 2020 Jul; 91(7):074501. PubMed ID: 32752859
    [TBL] [Abstract][Full Text] [Related]  

  • 31. A high sensitivity momentum flux measuring instrument for plasma thruster exhausts and diffusive plasmas.
    West MD; Charles C; Boswell RW
    Rev Sci Instrum; 2009 May; 80(5):053509. PubMed ID: 19485509
    [TBL] [Abstract][Full Text] [Related]  

  • 32. Development of a high dynamic range retarding potential analyzer for electric propulsion plume diagnosis.
    Maystrenko D; Shagayda A; Kravchenko D; Lovtsov A
    Rev Sci Instrum; 2022 Jul; 93(7):073504. PubMed ID: 35922286
    [TBL] [Abstract][Full Text] [Related]  

  • 33. Comparison of azimuthal ion velocity profiles using Mach probes, time delay estimation, and laser induced fluorescence in a linear plasma device.
    Thakur SC; McCarren D; Lee T; Fedorczak N; Manz P; Scime EE; Tynan GR; Xu M; Yu J
    Rev Sci Instrum; 2012 Oct; 83(10):10D708. PubMed ID: 23126882
    [TBL] [Abstract][Full Text] [Related]  

  • 34. Development of a 50-A heaterless hollow cathode for electric thrusters.
    Payman AR; Goebel DM
    Rev Sci Instrum; 2022 Nov; 93(11):113543. PubMed ID: 36461510
    [TBL] [Abstract][Full Text] [Related]  

  • 35. Electron temperature measurement in Maxwellian non-isothermal beam plasma of an ion thruster.
    Zhang Z; Tang H; Kong M; Zhang Z; Ren J
    Rev Sci Instrum; 2015 Feb; 86(2):023506. PubMed ID: 25725841
    [TBL] [Abstract][Full Text] [Related]  

  • 36. A high power ion thruster for deep space missions.
    Polk JE; Goebel DM; Snyder JS; Schneider AC; Johnson LK; Sengupta A
    Rev Sci Instrum; 2012 Jul; 83(7):073306. PubMed ID: 22852684
    [TBL] [Abstract][Full Text] [Related]  

  • 37. A survey of propulsion options for cargo and piloted missions to Mars.
    Sankaran K; Cassady L; Kodys AD; Choueiri EY
    Ann N Y Acad Sci; 2004 May; 1017():450-67. PubMed ID: 15220162
    [TBL] [Abstract][Full Text] [Related]  

  • 38. Thirty percent conversion efficiency from radiofrequency power to thrust energy in a magnetic nozzle plasma thruster.
    Takahashi K
    Sci Rep; 2022 Nov; 12(1):18618. PubMed ID: 36357485
    [TBL] [Abstract][Full Text] [Related]  

  • 39. Laser-heated emissive plasma probe.
    Schrittwieser R; Ionita C; Balan P; Gstrein R; Grulke O; Windisch T; Brandt C; Klinger T; Madani R; Amarandei G; Sarma AK
    Rev Sci Instrum; 2008 Aug; 79(8):083508. PubMed ID: 19044350
    [TBL] [Abstract][Full Text] [Related]  

  • 40. Improving the viability and versatility of the E × B probe with an active cooling system.
    Liu L; Cai G; You F; Ren X; Zheng H; He B
    Rev Sci Instrum; 2018 Apr; 89(4):043502. PubMed ID: 29716320
    [TBL] [Abstract][Full Text] [Related]  

    [Previous]   [Next]    [New Search]
    of 7.