[HTML][HTML] Hydrogen peroxide–A promising oxidizer for rocket propulsion and its application in solid rocket propellants

W Kopacz, A Okninski, A Kasztankiewicz… - FirePhysChem, 2022 - Elsevier
This paper discusses the potential use of hydrogen peroxide as oxidizer for solid rocket
propulsion. While hydrogen peroxide is a liquid in normal conditions, it may be used in solid …

Rocket‐Inspired Effervescent Motors for Oral Macromolecule Delivery

L Cai, G Chen, L Sun, S Miao, L Shang… - Advanced …, 2023 - Wiley Online Library
Oral administration is among the most convenient ways with good patient compliance for
drug delivery; while it remains a challenge to achieve desirable bioavailability of most …

Effects of hydrogen peroxide on the combustion and emissions of an ethanol/gasoline combined injection engine under different excess air ratios

J Zhang, P Sun, W Shi, X Yu, D Li, Y Li, T Wang, Z Zhao… - Fuel, 2024 - Elsevier
Abstract Hydrogen peroxide (H 2 O 2) can prompt hydroxyl radicals and chain reactions in
the combustion process. Compared with the research on compression ignition engines, the …

Research progress on the catalytic and thermal decomposition of ammonium dinitramide (ADN)

Y Tian, W Xu, W Cong, X Bi, J He, Z Song, H Guan… - RSC …, 2024 - pubs.rsc.org
Ammonium dinitramide (NH4N (NO3) 2, ADN) is regarded as a promising oxidizer due to its
low signature and high specific impulse. Generally, ADN undergoes exothermic …

Reduction of chemical mechanism and kinetics analysis for ignition of RP-3 aviation kerosene in partially catalyzed hydrogen peroxide

S Han, N Yu, G Cai, Z Zhao - Fuel, 2024 - Elsevier
Partial catalytic autoignition schemes for hydrogen peroxide (HP)/kerosene engines have
demonstrated considerable potential advantages; however, the kinetic process for the …

The chemical dynamics of hydrogen/hydrogen peroxide blends diluted with steam at compression ignition relevant conditions

EA Tingas - Fuel, 2021 - Elsevier
In the current work, the use of hydrogen peroxide as an additive to hydrogen/air mixtures is
proposed and explored computationally, in conditions relevant to compression ignition …

Integration validation of key components for small sounding rockets

Y Yun, J Seo, K Park, J Huh, J Lim, S Kwon - Aerospace Science and …, 2020 - Elsevier
To develop sounding rockets that can be used for various missions, a university, research
center, and two enterprises collaborated to conduct a critical-system development project on …

2.5 kN pump-pressure pintle engine ignition experiment in different loading cases

N Yu, C Zhou, G Cai, J Wang - Aerospace Science and Technology, 2022 - Elsevier
Advanced technology of motors and batteries has stimulated the application of the emerging
electric pump in the liquid propulsion systems. However, the coupling characteristics …

Design optimization of velocity-controlled cruise vehicle propelled by throttleable hybrid rocket motor

M Xiao, H Zhu, Z Du, Y Gao, H Tian, G Cai - Aerospace Science and …, 2021 - Elsevier
Throttleable engines have greatly raised the technical performances of aircrafts and
missiles, particularly for cruise vehicles. The hybrid rocket motor (HRM) combines the …

Flow field and injector heat characteristics of hybrid rocket motor with annular-gap injector

C Li, G Cai, P Wang, H Tian - Aerospace Science and Technology, 2019 - Elsevier
A throttleable annular-gap axial injector, which could automatically adjust the injection gap
area, is proposed to decrease injection pressure drop variation amplitude during wide range …