• 72 Citations
  • 5 h-Index
20032019
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Fingerprint Dive into the research topics where Jeffrey David Moore is active. These topic labels come from the works of this person. Together they form a unique fingerprint.

  • 4 Similar Profiles
Propellants Engineering & Materials Science
Rocket engines Engineering & Materials Science
rockets Physics & Astronomy
Propulsion Engineering & Materials Science
Ignition Engineering & Materials Science
fins Physics & Astronomy
slots Physics & Astronomy
flames Physics & Astronomy

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Research Output 2003 2019

  • 72 Citations
  • 5 h-Index
  • 14 Conference contribution
  • 8 Article

Evaluation of orifice inlet geometries on single liquid injectors through cold-flow experiments

Kiaoulias, D. N., Travis, T. A., Moore, J. D. & Risha, G. A., May 1 2019, In : Experimental Thermal and Fluid Science. 103, p. 78-88 11 p.

Research output: Contribution to journalArticle

Orifices
Geometry
Liquids
Experiments
Pressure drop

Priming event peak pressures in liquid propulsion systems

Moore, J. D., Gilbert, J., Brindle, B. & Risha, G. A., Jan 1 2019, In : Journal of Spacecraft and Rockets. 56, 3, p. 899-909 11 p.

Research output: Contribution to journalArticle

priming
propulsion
Propulsion
propellants
water hammer

Evaluation of liquid propulsion system design on priming event pressure levels

Kiaoulias, D., Zvorsky, I., Ismail, S., Meyers, N., Bhalla, J. & Moore, J. D., Jan 1 2018, 2018 Joint Propulsion Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-4757. (2018 Joint Propulsion Conference).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Propulsion
Systems analysis
Liquids
Monopropellants
Water hammer

Activation time analysis in a propulsion system

Moore, J. D., Jan 1 2017, 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA, (53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Propulsion
Chemical activation
Propellants
Orifices
Hydrazine

Development of 10 inch diameter titanium rolling metal diaphragm tank for green propellant

Conomos, H., Alongi, C. G., Yager, J., Goddard, R. A., Salzler, T. J., Fetes, J. P., Burch, K. J. & Moore, J. D., Jan 1 2017, 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA, (53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Propellants
Diaphragms
Titanium
Metals
Dynamic response