High-Frequency Supersonic Heating of Hydrogen for Propulsion

Bonneville, Jacques M.

doi:10.2514/6.1963-26

Electric Propulsion Conference 1963

DOI: 10.2514/6.1963-26

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High-Frequency Supersonic Heating of Hydrogen for Propulsion

Jacques M. Bonneville

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2009

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Velocity and total pressure measurements in the two-stage hybrid thruster tihtus

Böhrk¹,

Auweter‐Kurtz²

2009

Progress in Propulsion Physics

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A novel two-stage thermal-inductive hybrid thruster of the Universitat Stuttgart (TIHTUS) is under development at the Institut fur Raumfahrtsysteme (IRS). It provides the possibility to supply power and mass- §ow through either stage into the plasma. A variation of power-and mass§ow-staging was investigated with a Pitot probe and an electric timeof- §ight probe. The present paper discloses the radially resolved measurement results of total pressure and plasma velocity at a downstream position of 200 mm. Furthermore, a method is presented to access radially resolved §ow temperature from the combined pressure and velocity measurement. The temperature data are also presented. For a sum of powers of 50 kW at 300 mg/s, the Pitot pressure maximum is at 85 Pa while maximum velocity is measured as 9,224 and 10,350 m/s for two respective conditions. On the plume axis, the temperatures reach up to 9000 K.

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Velocity and total pressure measurements in the two-stage hybrid thruster tihtus

Böhrk¹,

Auweter‐Kurtz²

2009

Progress in Propulsion Physics

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TIHTUS Thrust Measurement with a Baffle Plate

Böhrk¹,

Auweter‐Kurtz²

2007

43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference &Amp;amp; Exhibit

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High-Frequency Supersonic Heating of Hydrogen for Propulsion

Cited by 2 publications

References 1 publication

Velocity and total pressure measurements in the two-stage hybrid thruster tihtus

Velocity and total pressure measurements in the two-stage hybrid thruster tihtus

TIHTUS Thrust Measurement with a Baffle Plate

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