SMORE Phase 2: An Upgrade in Valve Systems & Startup Procedure for A Small Methanol Oxygen Liquid Rocket Engine
ثبت نشده
چکیده
منابع مشابه
Specific Impulse and Ignition Delay Time Assessment for DMAZ with Liquid Oxidizers for an Upper Stage Rocket Engine
2-Dimethyl amino ethyl azide (DMAZ) has attracted much attention as a suitable liquid fuel replacement for monomethyl hydrazine (MMH) and unsymmetrical dimethyl hydrazine (UDMH) in propellant systems because, in contrast to these fuels, it is noncarcinogen. In this research, performance, and ignition delay time of DMAZ were studied with common liquid oxidizers such as inhibited red fuming n...
متن کاملA New Approach to Flow Network Analysis of an Engine Lubrication System
In order to develop more efficient engines, it is essential to optimize the lubrication circuit of the power train systems. In this paper, during an engine design and development process, a network analysis of the engine lubrication system is described in detail. Two elements have been added to the lubrication circuit in the modified engine. These elements are hydraulic lifters and an Anti-d...
متن کاملمرروری بر روشهای تولید آمونیوم دینیترآمید ((ADN و توسعه کاربردی آن در پیشرانش فضایی
Owing to the prime importance of ammonium dinitramide (ADN) as an oxidizer in solid propellants, its synthesis has received a great amount of interest. There have been several new and innovative synthesis routes developed by researcher’s worldwide. Liquid-fuel rockets consist of a fuel and oxygen (or other oxidizer) in liquid state. These fractals are already being combined together or combined...
متن کاملEmission Reduction Strategies for Small Single Cylinder Diesel Engine Using Valve Timing and Swirl Ratio
Small diesel engines are widely used for commercial vehicle and passenger car applications due to their higher torque requirements, fuel economy, and better thermal efficiency. These engines are exposed to different operating and environmental conditions and hence emissions from these engines are erratic. Strategies are required to enhance performance and reduce engine-out emissions considering...
متن کاملآتشزنهها در سیستمهای پیشرانش مایع غیرخود مشتعل شونده
Liquid propulsion systems have effective role in implementation of space and military mission due to high performance and specific impulse. Liquid propellants are divided into two categories: hypergolic and non-hypergolic propellants. Non-hypergolic propellants need an igniter system to provide the initial energy for propellant ignition compared with hypergolic propellants. Since failure in ign...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
عنوان ژورنال:
دوره شماره
صفحات -
تاریخ انتشار 2010