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    Wall heat transfer prediction in CH4/O2 and H2/O2 rocket thrust chambers using a non-adiabatic flamelet model

    Perakis, Nikolaos / Haidn, Oskar J. | Elsevier | 2020

    Theoretical Thermodynamic Data and Calculations of Performance of the Rocket Propellant System H 2/ O 2 for a Chamber Pressure of 0.484 KP/Sq cm

    W. Buschulte / H. Koch | NTIS | 1969

    The OH and H2O masers in the starbust galaxy messier 82

    Baudry, A. / Diamond, P. / Henkel, C. | Elsevier | 1991

    The Lunar H~2/O Resource Use Program Plan

    Rice, E. E. / Gustafson, R. J. / Teeter, R. R. et al. | British Library Conference Proceedings | 2000

    TDLAS a laser diode sensor for the in situ monitoring of H2O, CO2 and their isotopes in the Martian atmosphere

    Barbu, T. Le / Vinogradov, I. / Durry, G. et al. | Elsevier | 2005

    Suppression of Hard Start for Nontoxic Hypergolic Thruster Using H 2 O 2 Oxidizer

    Kang, Hongjae / Lee, Eunkwang / Kwon, Sejin | AIAA | 2017

    Sunfire – Erneuerbare Moleküle aus CO2 und H2O zur Substitution von Erdöl und Erdgas

    Power to X – Full integration of renewables into all sectors
    von Olshausen, Christian / Hauptmeier, Karl | Springer Verlag | 2019

    Room-temperature catalytically reactive ammonium dinitramide–H2O2 monopropellant for microsatellites

    Kim, Ju Won / Bhosale, Vikas Khandu / Kim, Kyu-Seop et al. | Elsevier | 2021

    Regression Rate and Performance Analysis via Ballistic Reconstruction of a small-scale H2O2-based Hybrid Rocket fuelled by Polyvinyl Chloride

    Cassese, S. / Mungiguerra, S. / Guida, R. et al. | Elsevier | 2024

    Reduction of Catalyst Volume by Using Metal Mesh in Small-Scale H 2 O 2 Thrusters

    Lee, Jeongsub / Kwon, Sejin | AIAA | 2013

    Radiation stability of organic matter in liquid and frozen H2O, NH3 and water-ammonia mixtures

    Nebeling, B. / Roessler, K. / Schmitz, G. | Elsevier | 1987

    Preliminary Study of Graphite Rod Pre-treatment in H2O2/H2SO4 Mixture Solution on the Synthesized Graphene by Electrochemical Exfoliation Method

    Iskandar, Ferry / Abdillah, Oktaviardi Bityasmawan / Mayangsari, Tirta Rona et al. | IEEE | 2018

    Preheating characteristics of H2O2 monopropellant thruster using manganese oxide catalyst

    Jang, Dongwook / Kang, Shinjae / Kwon, Sejin | Elsevier | 2014

    Performance of Dicyclopentadiene/ H 2 O 2 -Based Hybrid Rocket Motors with Metal Hydride Additives

    Shark, S. C. / Pourpoint, T. L. / Son, S. F. et al. | AIAA | 2013

    Performance Assessment of 1 N Bipropellant Thruster Using Green Propellants H 2 O 2 / Kerosene

    Krejci, David / Woschnak, Alexander / Scharlemann, Carsten et al. | AIAA | 2012

    P8 - The New French/German Research Test Facility for H~2/O~2 - High Pressure Rocket Engine Combustion Devices

    Haidn, O. J. / Stratmann, K. / Vuillermoz, P. et al. | British Library Conference Proceedings | 1995

    Optimization of a Catalytic Chamber for H 2 O 2 Decomposition Based on Beads

    Quintens, Hugo / Boust, Bastien / Bellenoue, Marc et al. | AIAA | 2022

    Numerical Studies on Multidimensional H~2/O~2/N~2 Premixed Jet Flame

    Katta, V. R. / Roquemore, W. M. / AIAA | British Library Conference Proceedings | 1994

    Numerical Simulation of Magnetohydrodynamics Natural Convection of CuO - H 2 O Nanofluid Inside Circular Enclosure

    Ren, Jiyun / Jin, Ruibo / Liu, Yang et al. | AIAA | 2022

    Numerical Investigation of Cu–H2O Nanofluid in a Differentially Heated Square Cavity with Conducting Square Cylinder Placed at Arbitrary Locations

    Kumar, Basant / Sharma, Bishwajit / Barman, Rabindra Nath | Springer Verlag | 2018

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