В.И. Захаров, Е.Ю. Локтионов, Ю.С. Протасов, Ю.Ю. Протасов
18
[20]
Jamison A.J., Ketsdever A.D., Muntz E.P. Accurate Measurement of Nano-Newton
Thrust for Micropropulsion System Characterization.
27th International Electric
Propulsion Conference
. Pasadena, 2001, p. IEPC-01-236.
[21]
Pottinger S.J., Lamprou D., Knoll A.K., Lappas V.J. Impact of plasma noise on
a direct thrust measurement system.
Review of Scientific Instruments
, 2012, vol.
83, no. 3, p. 033504.
[22] Kremeyer K. Ultrashort pulse lasers applied to propulsion/control in space- and
atmospheric-flight.
High-Power Laser Ablation VII
. Taos, NM, USA, SPIE,
2008, p. 700506–17.
[23] Cubbin E.A., Ziemer J.K., Choueiri E.Y., Jahn R.G. Pulsed thrust
measurements using laser interferometry.
Review of Scientific Instruments
,
1997, vol. 68, no. 6, pp. 2339–2346.
[24]
Polzin K.A., Markusic T.E., Stanojev B.J., DeHoyos A., Spaun B. Thrust stand
for electric propulsion performance evaluation.
Review of Scientific
Instruments
, 2006, vol. 77, no. 10, p. 105108-9.
[25] Choi S., Han T.-h., Gojani A., Yoh J. Thrust enhancement via gel-type liquid
confinement of laser ablation of solid metal propellant.
Applied Physics A
,
2010, vol. 98, no. 1, pp. 147–151.
[26] Kremeyer K., Lapeyre J., Hamann S. Compact And Robust Laser Impulse
Measurement Device, With Ultrashort Pulse Laser Ablation Results.
Fifth
International Symposium on Beamed Energy Propulsion
. Kailua-Kona
(Hawaii), AIP, 2008, pp. 147–158.
[27]
Eckel H.-A., Schall W., Walther S.
Lightcraft Impulse Measurements under
Vacuum
. DLR, 2003, 72 p.
[28] Michaelis M.M., Moorgawa A., Forbes A., Klopper W., McKenzie E.,
Boutchiama D., Bencherif H. Laser propulsion experiments in South Africa.
High-Power Laser Ablation IV
. Taos, NM, USA, SPIE, 2002, pp. 691–699.
[29] Watanabe K., Takahashi T., Sasoh A. Useful In-space Impulse Generation
Powered by Laser Energy.
Second International Symposium on Beamed Energy
Propulsion
. Sendai (Japan), AIP, 2004, pp. 115–121.
[30] Myrabo L.N. Brief History of the Lightcraft Technology Demonstrator (LTD)
Project.
First International Symposium on Beamed Energy Propulsion
.
Huntsville, Alabama (USA), AIP, 2003, pp. 49–60.
[31] Watanabe K., Sasoh A. Impulse Generation Using 300-J Class Laser with
Confinement Geometries in Air.
Transactions of the Japan Society for
Aeronautical and Space Sciences
, 2005, vol. 48, no. 159, pp. 49–52.
[32]
Shi L., Zhao S.-H., Chu X.-C., Ma L.-H., Wu J.-L., Li X.-L., Li Y.-J. Effect of
a simple double-confined structure on nanosecond pulse ablative laser
propulsion.
Europhysics Letters
, 2009, vol. 85, no. 5, p. 55001.
[33] Gamero-Castaño M., Hruby V., Martínez-Sánchez M. A Torsional Balance that
Resolves Sub-micro-Newton Forces.
27th International Electric Propulsion
Conference
. Pasadena, 2001, p. IEPC-01-235.
[34]
Selden N.P., Ketsdever A.D. Comparison of force balance calibration
techniques for the nano-Newton range.
Review of Scientific Instruments
, 2003,
vol. 74, no. 12, pp. 5249–5254.
[35]
Pancotti A.P., Gilpin M., Hilario M.S. Comparison of electrostatic fins with
piezoelectric impact hammer techniques to extend impulse calibration range of
a torsional thrust stand.
Review of Scientific Instruments
, 2012, vol. 83, no. 3,
p. 035109.
