39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Latest Publications

TOTAL DOCUMENTS

669

(FIVE YEARS 0)

H-INDEX

(FIVE YEARS 0)

Published By American Institute Of Aeronautics And Astronautics

9781624100987

Latest Documents Most Cited Documents Contributed Authors Related Sources Related Keywords

Development Status of the VINCI Engine of the ARIANE 5 Upper Stage

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit ◽

10.2514/6.2003-4484 ◽

2003 ◽

Cited By ~ 6

Author(s):

Patrick Alliot ◽

Eric Dalbies ◽

Jean-Marc Ruault

Keyword(s):

Development Status ◽

Upper Stage

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Microsecond Timescale Surface Temperature Measurements in Micro Pulsed Plasma Thrusters

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit ◽

10.2514/6.2003-5167 ◽

2003 ◽

Cited By ~ 1

Author(s):

Erik Antonsen ◽

Rodney Burton ◽

Gregory Spanjers ◽

Ronald Spores

Keyword(s):

Surface Temperature ◽

Temperature Measurements ◽

Pulsed Plasma ◽

Pulsed Plasma Thrusters ◽

Plasma Thrusters

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Assessing Model Uncertainty in the Conceptual Design of a Monopropellant Propulsion System

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit ◽

10.2514/6.2003-4470 ◽

2003 ◽

Cited By ~ 3

Author(s):

Daniel Thunnissen ◽

Carl Engelbrecht ◽

Jeffrey Weiss

Keyword(s):

Conceptual Design ◽

Model Uncertainty ◽

Propulsion System

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Flash-Evaporation of Oxidizer Spray During Start-Up of an Upper-Stage Rocket Engine

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit ◽

10.2514/6.2003-5075 ◽

2003 ◽

Cited By ~ 5

Author(s):

Roland Schmehl ◽

Johan Steelant

Keyword(s):

Rocket Engine ◽

Flash Evaporation ◽

Start Up ◽

Upper Stage

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LES of Fuel Jet in Cross-Flow Using Lattice Boltzmann Method

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit ◽

10.2514/6.2003-5206 ◽

2003 ◽

Cited By ~ 1

Author(s):

Homayoon Feiz ◽

Suresh Menon

Keyword(s):

Lattice Boltzmann Method ◽

Lattice Boltzmann ◽

Cross Flow ◽

Jet In Cross Flow ◽

Fuel Jet ◽

Boltzmann Method

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Comparison of Planar and Axisymmetric Flowpaths for Hydrogen Fueled (invited)

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit ◽

10.2514/6.2003-4407 ◽

2003 ◽

Cited By ~ 4

Author(s):

Fred Billig ◽

Lance Jacobsen

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Precision Adjustable Liquid Regulator

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit ◽

10.2514/6.2003-4610 ◽

2003 ◽

Author(s):

Richard Meinhold ◽

Morgan Parker

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Future Space Propulsion Based on Heim's Field Theory

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit ◽

10.2514/6.2003-4990 ◽

2003 ◽

Cited By ~ 4

Author(s):

Walter Dröscher ◽

Jochem Hauser

Keyword(s):

Field Theory ◽

Space Propulsion ◽

Future Space

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Electrostatically Actuated Fuel Atomizer Design for the Pulse Detonation Engine

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit ◽

10.2514/6.2003-4821 ◽

2003 ◽

Cited By ~ 1

Author(s):

James Nabity ◽

Gino Balducci ◽

John Daily

Keyword(s):

Pulse Detonation Engine ◽

Electrostatically Actuated ◽

Pulse Detonation ◽

Detonation Engine

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A Study on Premixed Turbulent Combustion of Hydrogen Including Hydrocarbon

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit ◽

10.2514/6.2003-4638 ◽

2003 ◽

Cited By ~ 2

Author(s):

Hiroyuki Kido ◽

Masaya Nakahara ◽

Kenshiro Nakashima

Keyword(s):

Turbulent Combustion ◽

Premixed Turbulent Combustion ◽

Combustion Of Hydrogen

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39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and ExhibitLatest Publications

TOTAL DOCUMENTS

H-INDEX

Published By American Institute Of Aeronautics And Astronautics

Development Status of the VINCI Engine of the ARIANE 5 Upper Stage

Microsecond Timescale Surface Temperature Measurements in Micro Pulsed Plasma Thrusters

Assessing Model Uncertainty in the Conceptual Design of a Monopropellant Propulsion System

Flash-Evaporation of Oxidizer Spray During Start-Up of an Upper-Stage Rocket Engine

LES of Fuel Jet in Cross-Flow Using Lattice Boltzmann Method

Comparison of Planar and Axisymmetric Flowpaths for Hydrogen Fueled (invited)

Precision Adjustable Liquid Regulator

Future Space Propulsion Based on Heim's Field Theory

Electrostatically Actuated Fuel Atomizer Design for the Pulse Detonation Engine

A Study on Premixed Turbulent Combustion of Hydrogen Including Hydrocarbon

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Latest Publications