Thermal Decomposition Kinetics of Kerosene-Based Rocket Propellants. 3. RP-2 with Varying Concentrations of the Stabilizing Additive 1,2,3,4-Tetrahydroquinoline-Reference-Cited by-同舟云学术

Thermal Decomposition Kinetics of Kerosene-Based Rocket Propellants. 3. RP-2 with Varying Concentrations of the Stabilizing Additive 1,2,3,4-Tetrahydroquinoline

Published:2010-12-08 Issue:1 Volume:25 Page:288-292
ISSN:0887-0624
Container-title:Energy & Fuels
language:en
Short-container-title:Energy Fuels

Author:

Widegren Jason A.¹,Bruno Thomas J.¹

Affiliation:

1. Thermophysical Properties Division, National Institute of Standards and Technology (NIST), 325 Broadway, Boulder, Colorado 80305-3328, United States

Publisher

American Chemical Society (ACS)

Subject

Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering

Link

https://pubs.acs.org/doi/pdf/10.1021/ef101376k

Reference30 articles.

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3. Laboratory-Scale Thermal Stability Experiments on RP-1 and RP-2

4. Thermal Stability of Energetic Hydrocarbon Fuels for Use in Combined Cycle Engines

5. Bates, R. W.; Edwards, T.; Meyer, M. L.Heat transfer and deposition behavior of hydrocarbon rocket fuels.Proceeding of the 41st Aerospace Sciences Meeting and Exhibit; Reno, NV, Jan 6−9, 2003; AIAA Paper 2003-123.

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