53rd AIAA/SAE/ASEE Joint Propulsion Conference
Latest Publications

TOTAL DOCUMENTS

419

(FIVE YEARS 0)

H-INDEX

(FIVE YEARS 0)

Published By American Institute Of Aeronautics And Astronautics

9781624105111

Latest Documents Most Cited Documents Contributed Authors Related Sources Related Keywords

Correction: Small-scale Gaseous Oxygen Hybrd Rocket Testing for Regression Rate and Combustion Efficiency Studies

53rd AIAA/SAE/ASEE Joint Propulsion Conference ◽

10.2514/6.2017-4643.c1 ◽

2017 ◽

Author(s):

Flora S. Mechentel ◽

A.M. Coates ◽

Brian J. Cantwell

Keyword(s):

Combustion Efficiency ◽

Small Scale ◽

Gaseous Oxygen ◽

Regression Rate

Download Full-text

Performance Characterization of Dusty Fuels to Investigate the In-Situ Resource Utilization Capabilities of a Pulsed Plasma Thruster System

53rd AIAA/SAE/ASEE Joint Propulsion Conference ◽

10.2514/6.2017-4607 ◽

2017 ◽

Cited By ~ 1

Author(s):

Michael Wennerstrom ◽

Brittney Dodson ◽

Robert Winglee ◽

Simon Fraser

Keyword(s):

Resource Utilization ◽

Pulsed Plasma ◽

Performance Characterization ◽

Pulsed Plasma Thruster ◽

Plasma Thruster

Download Full-text

Air-Breathing Pulsed Plasma Thruster with a Variable Spacing Cathode for Atmospheric Satellite Applications

53rd AIAA/SAE/ASEE Joint Propulsion Conference ◽

10.2514/6.2017-5039 ◽

2017 ◽

Cited By ~ 1

Author(s):

Manuel Azuara Rosales ◽

Robert Winglee ◽

Paige Northway

Keyword(s):

Pulsed Plasma ◽

Air Breathing ◽

Pulsed Plasma Thruster ◽

Plasma Thruster ◽

Satellite Applications

Download Full-text

Development and Testing of SP7 Fuel for Mars Ascent Vehicle Application

53rd AIAA/SAE/ASEE Joint Propulsion Conference ◽

10.2514/6.2017-4831 ◽

2017 ◽

Cited By ~ 5

Author(s):

Brian J. Evans ◽

Arif M. Karabeyoglu

Download Full-text

Mission Design and Trade Study Considerations for Reactionless Thrusters

53rd AIAA/SAE/ASEE Joint Propulsion Conference ◽

10.2514/6.2017-4843 ◽

2017 ◽

Cited By ~ 1

Author(s):

Shae Williams

Keyword(s):

Mission Design ◽

Trade Study

Download Full-text

Arc-Ignition of a 70%-85% Hydrogen Peroxide/ABS Hybrid Rocket System

53rd AIAA/SAE/ASEE Joint Propulsion Conference ◽

10.2514/6.2017-5047 ◽

2017 ◽

Cited By ~ 3

Author(s):

Stephen A. Whitmore ◽

Daniel P. Merkley

Keyword(s):

Hydrogen Peroxide ◽

Hybrid Rocket ◽

Rocket System

Download Full-text

Optimization of blades stagger angles of the three-spool axial compressor to improve of efficiency of the gas turbine engine

53rd AIAA/SAE/ASEE Joint Propulsion Conference ◽

10.2514/6.2017-4733 ◽

2017 ◽

Author(s):

Igor Egorov ◽

Evgeny Marchukov ◽

Grigorii Popov ◽

Oleg Baturin ◽

Evgenii Goriachkin ◽

...

Keyword(s):

Gas Turbine ◽

Axial Compressor ◽

Gas Turbine Engine ◽

Turbine Engine

Download Full-text

Propulsion Curriculum and Research in the Aerospace Engineering Department at the University of Maryland

53rd AIAA/SAE/ASEE Joint Propulsion Conference ◽

10.2514/6.2017-4881 ◽

2017 ◽

Author(s):

Raymond J. Sedwick ◽

Christopher P. Cadou ◽

Kenneth Yu

Keyword(s):

Aerospace Engineering ◽

University Of Maryland ◽

Engineering Department ◽

The University

Download Full-text

Extinction Conditions of Low-Speed Ballistic Bluff-Body Stabilized Flames

53rd AIAA/SAE/ASEE Joint Propulsion Conference ◽

10.2514/6.2017-4775 ◽

2017 ◽

Author(s):

Christian Engelmann ◽

Marissa K. Geikie ◽

Anthony J. Morales ◽

Kareem Ahmed

Keyword(s):

Bluff Body ◽

Low Speed ◽

Stabilized Flames

Download Full-text

Research Capability in Combustion and Propulsion at the Georgia Institute of Technology

53rd AIAA/SAE/ASEE Joint Propulsion Conference ◽

10.2514/6.2017-4803 ◽

2017 ◽

Cited By ~ 1

Author(s):

David R. Jovel ◽

Mitchell L. Walker ◽

Vigor Yang

Keyword(s):

Georgia Institute ◽

Institute Of Technology

Download Full-text

53rd AIAA/SAE/ASEE Joint Propulsion ConferenceLatest Publications

TOTAL DOCUMENTS

H-INDEX

Published By American Institute Of Aeronautics And Astronautics

Correction: Small-scale Gaseous Oxygen Hybrd Rocket Testing for Regression Rate and Combustion Efficiency Studies

Performance Characterization of Dusty Fuels to Investigate the In-Situ Resource Utilization Capabilities of a Pulsed Plasma Thruster System

Air-Breathing Pulsed Plasma Thruster with a Variable Spacing Cathode for Atmospheric Satellite Applications

Development and Testing of SP7 Fuel for Mars Ascent Vehicle Application

Mission Design and Trade Study Considerations for Reactionless Thrusters

Arc-Ignition of a 70%-85% Hydrogen Peroxide/ABS Hybrid Rocket System

Optimization of blades stagger angles of the three-spool axial compressor to improve of efficiency of the gas turbine engine

Propulsion Curriculum and Research in the Aerospace Engineering Department at the University of Maryland

Extinction Conditions of Low-Speed Ballistic Bluff-Body Stabilized Flames

Research Capability in Combustion and Propulsion at the Georgia Institute of Technology

53rd AIAA/SAE/ASEE Joint Propulsion Conference
Latest Publications