Reference health

The auto-ignition boundary of ethylene/nitrous oxide as a promising monopropellant

https://doi.org/10.1016/j.combustflame.2020.07.024
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21/21 checkable references clean · checked 2026-07-22

Every reference with a DOI in the deposited reference list resolved to a known work in Crossref or DataCite at the dated check, and none carried a retraction, withdrawal, or removal notice.

10 without a DOI — not checked. A reference deposited without a DOI is never matched by title or guessed at; it stays outside the checked set, and this line discloses that.

The 21 checked references that resolve
resolves10.2514/1.B35086
Green Propulsion Advancement: Challenging the Maturity of Monopropellant Hydrazine
resolves10.1016/j.paerosci.2014.08.001
Green space propulsion: Opportunities and prospects
resolves10.1007/s12567-015-0109-x
Enhanced development of a catalyst chamber for the decomposition of up to 1.0 kg/s hydrogen peroxide
resolves10.1134/S001050821205005X
HAN-based green propellant, application, and its combustion mechanism
resolves10.2514/1.B34341
Assessment of Imidazole-Based Ionic Liquids as Dual-Mode Spacecraft Propellants
resolves10.1039/c0cc02162h
Catalytic ignition of ionic liquids for propellant applications
resolves10.2514/1.47131
Engineering Model for Self-Pressurizing Saturated-N2O-Propellant Feed Systems
resolves10.2514/1.B37391
Deflagration-to-Detonation Transition in Nitrous Oxide/Oxygen-Fuel Mixtures for Propulsion
resolves10.1016/j.combustflame.2019.01.011
Laminar burning velocities of C2H4/N2O flames: Experimental study and its chemical kinetics mechanism
resolves10.1007/s00193-014-0509-4
Ignition delay-time behind reflected shock waves of small hydrocarbons–nitrous oxide(–oxygen) mixtures
resolves10.2514/1.38451
Physical Hypothesis for the Combustion Instability in Cryogenic Liquid Rocket Engines
resolves10.2514/1.B34643
Modeling of Jet A1-H2O2 Autoignition in a Microrocket Combustion Chamber
resolves10.1016/j.jhazmat.2019.05.036
Auto-ignition behaviors of nitromethane in diluted oxygen in a rapid compression machine: Critical conditions for ignition, ignition delay times measurements, and kinetic modeling interpretation
resolves10.1016/j.fuel.2019.04.030
Promoting “adiabatic core” approximation in a rapid compression machine by an optimized creviced piston design
resolves10.1080/00102200600671898
A RAPID COMPRESSION MACHINE FOR CHEMICAL KINETICS STUDIES AT ELEVATED PRESSURES AND TEMPERATURES
resolves10.1016/j.proci.2016.07.075
Ignition delay times of low alkylfurans at high pressures using a rapid compression machine
resolves10.1016/j.combustflame.2014.04.014
Effects of buffer gas composition on low temperature ignition of iso-octane and n-heptane
resolves10.1016/j.combustflame.2018.08.006
An experimental and chemical kinetic modeling study of 1,3-butadiene combustion: Ignition delay time and laminar flame speed measurements
resolves10.1016/j.pecs.2018.01.002
Modeling nitrogen chemistry in combustion
resolves10.1021/acs.energyfuels.7b01425
Comparative Study of the Effects of Nitrous Oxide and Oxygen on Ethylene Ignition
resolves10.1016/0010-2180(88)90086-7
Ignition processes in hydrogenoxygen mixtures
The 10 references without a DOI — listed, not checked
no DOI — not checkedDevelopment and test of a 3D printed hydrogen peroxide flight control thruster
no DOI — not checkedA premixed green propellant consisting of N2O and C2H4: experimental analysis of quenching diameters to design flashback arresters
no DOI — not checkedPressure drop measurement of porous materials: flashback arrestors for a N2O/C2H4 premixed green propellant
no DOI — not checkedDetonation limits and velocity deficits of CH4, C2H4, C2H6 and C3H8 with N2O in a small diameter tube
no DOI — not checkedNOFBTM: a non-toxic, “Green” propulsion technology with high performance and low cost
no DOI — not checkedExperimental performance analysis (c* & c* efficiency) of a premixed green propellant consisting of N2O and C2H4
no DOI — not checkedCharacterization of hydrocarbon/nitrous oxide propellant combinations
no DOI — not checkedEthene/dinitrogen oxide - A green propellant to substitute hydrazine: investigation on its ignition delay time and laminar flame speed
no DOI — not checkedAutoignition of kerosene by decomposed peroxide in a dump combustor configuration
no DOI — not checkedR. Design, Chemkin, 2006URL:http://www.reactiondesign.com/products/chemkin.
What this badge says. CiteStamped means the CHECKABLE references of this work were clean at the dated check: each resolved to a known work in a public registry, and none carried a retraction notice at that time. It says nothing about the quality, findings, or importance of the work itself, and nothing about references deposited without a DOI.

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