Article
Plasma Investigations
2020. V. 58. № 2. P. 162–165
Kotel'nikov V.A., Kotelnikov M.V., Kassin D.V.
Probe measurements on board a hypersonic aircraft
The features of probe measurements on a hypersonic aircraft, the design of the probe block and its location on a hypersonic aircraft, and the processing technique of the obtained current-voltage characteristics are discussed. Original processing techniques are proposed, and some results of probe measurements, covering both the plasma parameters in the combustion products of a liquid propellant rocket engine and the parameters of the plasma arising at supersonic speeds near the hypersonic aircraft wall, are presented.
Article reference:
Kotel'nikov V.A., Kotelnikov M.V., Kassin D.V. Probe measurements on board a hypersonic aircraft, High Temp., 2020. V. 58. № 2. P. 162
Kotel'nikov V.A., Kotelnikov M.V., Kassin D.V. Probe measurements on board a hypersonic aircraft, High Temp., 2020. V. 58. № 2. P. 162