Covalent Organic Frameworks for Photocatalytic Hydrogen Peroxide Evolution
Chemistry – A European Journal, Volume 31, Issue 15, March 12, 2025.Τhis Review presents a comprehensive overview of the very recent developments on COF‐based photocatalysts for H2O2 evolution. First, neat COFs with variable architecture are critically explored, followed by the presentation of the most promising hybrid COF‐based heterojunctions.
Andreas Katsamitros +4 more
wiley +1 more source
Autophage engines: towards a throttleable solid motor [PDF]
, 2018 This paper describes the instrumented test firing of a rocket that seeks to combine the throttleability of a liquid-fueled engine with the simplicity of a solid motor.
Dron, Mykola +5 more
core +1 more source
Development Status of the L75: A Brazilian Liquid Propellant Rocket Engine
Journal of Aerospace Technology and Management, 2014 This paper provides an overview of the design and development process of the L75 Liquid Propellant Rocket Engine (LPRE). Being developed at Institute of Aeronautics and Space (IAE), it is the first Brazilian open-cycle liquid rocket engine pressurized by
Daniel Soares de Almeida +1 more
doaj
Model Rocket Project for Aerospace Engineering Course: Trajectory Simulation and Propellant Analysis [PDF]
arXiv, 2017 Model rockets have been employed in student projects, but very few papers in aerospace education offer concise summaries of activities at university-course levels. This paper aims to address this gap in the literature. The rockets used by our students reached some 500 m (~1,640 feet) in altitude, deployed a parachute, and spent 2-3 minutes descending ...
arxiv
Nonlinear Aspects of Combustion Instability in Liquid Propellant Rocket Motors. Second Yearly Progress Report for the Period 1 June 1961 to 31 May 1962 [PDF]
Combustion instability in liquid-propellant rocket ...
Harrje, D. T. +2 more
core +1 more source
Cooling process of liquid propellant rocket by means of kerosene-alumina nanofluid
Propulsion and Power Research, 2016 Heat transfer augmentation of kerosene-alumina nanofluid is studied for the possible use in the regenerative cooling channel of semi cryogenic engine.
Mostafa Mahmoodi, Sh. Kandelousi
doaj +1 more source
Integrated design optimization of structural bending filter and gain schedules for rocket attitude control system [PDF]
arXiv, 2018 This paper proposes an integrated design optimization framework for the gain schedules and bending filter for the longitudinal control of a rocket during its ascent flight. Dynamic models representing the pitch/yaw motion of a rocket considering the elements such as the rigid body dynamics, aerodynamics, sloshing, bending, sensor/actuator, and flight ...
arxiv
Eurasian Chemico-Technological Journal, 2017 Technogeneous impact of rocket and space activities on the environment is one of the most actual problems of practical cosmonautics. This technogeneous impact is not only the pollution of near Earth space with space debris (worked-off stages of space ...
V. Trushlyakov +2 more
doaj +1 more source
The alleged contributions of Pedro E. Paulet to liquid-propellant rocketry [PDF]
The first practical working liquid propellant rocket motor was claimed by Pedro E. Paulet, a South American engineer from Peru (1895). He operated a conical motor, 10 centimeters in diameter, using nitrogen peroxide and gasoline as propellants and ...
Ordway, F. I., III
core +1 more source
Servo-Stabilization of Low-Frequency Oscillations in a Liquid Bipropellant Rocket Motor [PDF]
, 1953 The recent work of H. S. Tsien concerning the servostabilization of rocket motors is extended to the liquid bipropellant rocket motor. It is shown that by use of a feedback system containing a device to sense the combustion chamber pressure, a suitably ...
Cox, Dale W., Jr., Marble, Frank E.
core +1 more source