Results 61 to 70 of about 39,486 (297)
Hypergolic droplet‒film interaction dynamics at high temperatures
Droplet, Volume 4, Issue 3, July 2025.The whole reaction process can be distinctly identified as three stages based on the corona size and the temperature temporal evolution. In the coalescence regime, T* maintains quasi‐stationary values during initial contact, corresponding to hydrodynamic coalescence process. Consequently, the first stage is defined as the inertia‐dominant stage. In the
Yuxin Song, Zuohua Huang, Chenglong Tang
wiley +1 more source
MATEC Web of Conferences, 2017 A method for increasing the safe explosion of the spent orbital stages of a space launch vehicle (SLV) with a propulsion rocket engine (PRE) based on the gasification of unusable residues propellant and venting fuel tanks.
Trushlyakov Valeriy I. +1 more
doaj +1 more source
Propellants, Explosives, Pyrotechnics, Volume 50, Issue 7, Page 106-114, July 2025.ABSTRACT The decomposition mechanisms of double base rocket propellants are well known and reported, but the influence of atmospheric conditions such as water and oxygen is poorly understood. In this work, the influence of water and oxygen on an extruded double base (EDB) rocket propellant aged between 70 and 100°C was examined using heat flow ...
Alonso Romero Jabalquinto +4 more
wiley +1 more source
Modeling of Shutdown Process in Liquid Propellant Rocket Engines [PDF]
فصلنامه علوم و فناوری فضایی, 2014 The effects of liquid propellant rocket engines thrust termination transients are important in achieving the launch vehicle’s desired final velocity with the required precision.
M. Shafiey Dehaj +4 more
doaj
Propellants, Explosives, Pyrotechnics, Volume 50, Issue 7, Page 11-30, July 2025.ABSTRACT Hydrazinium nitroformate (HNF) is a chlorine‐free, high‐energy oxidizer with promising applications in green propulsion systems. This review examines the thermal decomposition, combustion kinetics, flame structure, and behavior of HNF, while critically evaluating the current body of literature.
Lakshay Bansal +2 more
wiley +1 more source
Propellants, Explosives, Pyrotechnics, Volume 50, Issue 7, Page 95-105, July 2025.ABSTRACT The aerospace industry is continually seeking materials that offer higher performance and lower environmental impact. In chemical propulsion, ammonium dinitramide (ADN) represents a significant advance in this direction as a potential replacement for ammonium perchlorate in solid propellant formulations.
Josiane R. C. Silva +6 more
wiley +1 more source
High temperature spark plug Patent [PDF]
, 1966 High temperature spark plug for igniting liquid rocket ...
Watson, J. E.
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.
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International Journal of Urban and Regional Research, Volume 49, Issue 4, Page 757-778, July 2025.Abstract Data centers, the material backbone of smart cities, power the digital economy and advanced digital services. Metaphors of ‘the cloud’ and ‘cloud computing’ obscure the massive computing and storage infrastructures, the resource flows and the land uses they mediate.
Jochen Monstadt, Katherine Saltzman
wiley +1 more source
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