DocumentCode :
1719666
Title :
Spectroscopy measurements in rarefied plumes
Author :
Dankert, C. ; Dettleff, G. ; Nazari, B.K. ; Rosenhauer, M.
Author_Institution :
DLR Inst. for Fluid Mech., Gottingen, Germany
fYear :
2001
fDate :
8/1/2001 12:00:00 AM
Firstpage :
262
Lastpage :
271
Abstract :
In the DLR-high vacuum plume test facility STG experiments have been performed to study the expansion of plumes from small thrusters. The main feature of the chamber, a large liquid Helium driven cryopump, allows the undisturbed plume gas expansion into the highly rarefied regime including the backflow. Nitrogen was taken as test gas to generate a simple case without chemical reactions and a constant ratio of specific heats. The essential parameter was the nozzle flow Reynolds number, the quantities measured were the Pitot pressure at the nozzle exit, the molecule number flux in the plume, the rotational temperature and the density in the plume. The last two quantities were studied by REMPI-method (Resonance Enhanced Multi Photon Ionization) which delivers a precise determination of temperatures, density and the gas velocity. For the rotational temperature measurements in N2 the 2+2 REMPI at 283 nm was selected. The test conditions are po=0.5 bar to 2.0 bar, To=300 K, d*=0.6 mm, Re at the exit of the conical nozzle with, 15° throat 800 and 3200. The transitions S(0),... S(4) were taken for the determination of the rotational temperatures freezes at about 8 K. The flow field which could be studied by REMPI is pretty big; the detection limit was 2.5 m downstream on-axis, that corresponds to a density of 10-3 1/cm3 for N2-molecules
Keywords :
aerospace propulsion; aerospace test facilities; cryopumping; density measurement; flow measurement; ion engines; jets; multiphoton spectroscopy; nozzles; photoionisation; rarefied fluid dynamics; spectral methods of temperature measurement; 0.5 to 2 bar; 283 nm; 300 K; 8 K; Boltzmann rotational population distribution; N2; Pitot pressure; REMPI-method; conical nozzle; density measurements; flow field; free jet expansion; high vacuum plume test facility; highly rarefied regime; liquid helium driven cryopump; molecule number flux; nozzle flow Reynolds number; plume expansion; rarefied plumes; rotational temperature; satellite position control engines; small thrusters; Chemicals; Density measurement; Fluid flow measurement; Helium; Nitrogen; Performance evaluation; Spectroscopy; Temperature; Test facilities; Testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Instrumentation in Aerospace Simulation Facilities, 2001. 19th International Congress on ICIASF 2001
Conference_Location :
Cleveland, OH
Print_ISBN :
0-7803-7022-8
Type :
conf
DOI :
10.1109/ICIASF.2001.960259
Filename :
960259
Link To Document :
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