Timothée L. Pourpoint
Engineering · Purdue University West Lafayette
Publications
153
Citations
1,932
Est. group size
~7
Recurring co-author estimate
Active years
27
Publishing since 2000
Timothée L. Pourpoint's research focuses on rocket propulsion systems, particularly the chemistry and combustion behavior of propellants such as hydrazine-based and mixed oxides of nitrogen (green hypergolic propellants), and the design of experimental test facilities like optically accessible rocket engines and hypersonic test rigs. The work combines experimental measurements (e.g., density, surface tension, ignition delay) with hardware development for testing rocket engine components such as valves, injectors, and venturis. This research is relevant to students interested in aerospace engineering, propulsion, combustion science, and experimental fluid/thermodynamic characterization of rocket fuels.
Publication output peaked around 2019 and has generally declined since, with a gap in 2025 followed by a rebound in 2026, averaging under 4 papers per year over the last five years.
Generated by claude-sonnet-5 from public bibliographic data · Jul 20, 2026
- Design and Performance Analysis of an Optically Accessible Pneumatic Poppet Valve
2026
- Development of an Optically Accessible Green Hypergolic Rocket Engine with Bi Swirl Injector
2026
- Experimental and Numerical Study of an Optically Accessible Cavitating Venturi
2026
- KHz rate 3D white light particle tracking with a tunable acoustic gradient (TAG) lens
Optics Express · 2026
- Hydrazine-Based Green Monopropellant Blends
2024
- Hypersonic test facility using nitrous oxide
OSTI OAI (U.S. Department of Energy Office of Scientific and Technical Information) · 2024
- The Effect of Nitric Oxide on the Ignition Delay of Mixed Oxides of Nitrogen with Monomethylhydrazine
AIAA SCITECH 2023 Forum · 2023
- Density Characterization of Mixed Oxides of Nitrogen from Freezing Point to 50°C
AIAA SCITECH 2023 Forum · 2023
- Performance Evaluation of a Diffuser –Ejector System using Cold Gas Thrusters with Different Nozzle Geometries in the Purdue Altitude Chamber Facility
AIAA SCITECH 2023 Forum · 2023
- Surface Tension Measurements of Mixed Oxides of Nitrogen using Capillary Tubes
AIAA SCITECH 2023 Forum · 2023
- Speed of Sound Characterization of Mixed Oxides of Nitrogen from Freezing Point to 50°C
AIAA SCITECH 2023 Forum · 2023
- Coating Techniques for 3D Printed Catalyst Beds
AIAA SCITECH 2023 Forum · 2023
- Carbonaceous Deposit Density in a Fuel-Film-Cooled Rocket Combustor
Journal of Propulsion and Power · 2022
- Hypergolic Hybrid Rocket Engine Ignition and Relights with Mixed Oxides of Nitrogen
Journal of Propulsion and Power · 2021
- Carbonaceous Deposits in a Fuel-Film-Cooled Rocket Combustor: Optical Profilometry
Journal of Propulsion and Power · 2021
- Journal of Propulsion and Power×8
- AIAA Propulsion and Energy 2020 Forum×7
- Cambridge University Press eBooks×6
- AIAA Propulsion and Energy 2019 Forum×6
- AIAA SCITECH 2023 Forum×6
- Stephen D. Heister
Engineering · Purdue University West Lafayette
- Paul F. Penko
Engineering · The Ohio State University
- James Canino
Engineering · Purdue University West Lafayette
- William Anderson
Engineering · Purdue University West Lafayette
- Kyle E. Uhlenhake
Engineering · Purdue University West Lafayette
This profile was generated automatically from public scholarly data (OpenAlex). Group size and activity levels are estimates derived from co-authorship patterns.
Last updated Jul 20, 2026.
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