Results 111 to 120 of about 1,790,414 (217)

Test Campaign of a 10000 N Hybrid Rocket Engine

, 2015
A 10000 N hybrid rocket engine called HyRES (Hybrid Rocket Engine Stuttgart) is developed, built and tested by the student team Hybrid Engine development (HyEnD) at the University of Stuttgart within the DLR STERN program.
Kobald, Mario, Schmierer, C., Petrarolo, Anna   +2 more
core  

Combustion Characteristics of a Swirling LOX Type Hybrid Rocket Engine [PDF]

We have proposed a swirling oxidizer type hybrid rocket engine. In this paper, liquid oxygen (LOX) was used as oxidizer. Combustion tests of a hybrid rocket engine with a swirling LOX flow were conducted by changing the swirl strength. Ignition was rapid
キタガワ, コウキ, 41261644300, Yuasa, Saburo, 北川, 幸樹, 100001324, 湯浅, 三郎, Kitagawa, Koki, 10575476, 31326, 23865   +9 more
core  

Comparison of selected nozzles for hybrid rocket engine [PDF]

, 2019
Tato práce se zabývá tryskami pro daný malý hybridní raketový motor. Práce pokrývá teoretické výpočty, simulace, návrh konstrukce a výrobu trysek s různou geometrií.
Arjun Anil
core  

AN OPTIMIZED HYBRID ROCKET MOTOR FOR THE SARA PLATFORM REENTRY SYSTEM DOI 10.5028/jatm.2012.04032312

Journal of Aerospace Technology and Management, 2012
This paper has described a system design process, based on a multidisciplinary optimization technique, of a conceptual optimized hybrid propellant rocket motor. The proposed engine could be a technological option for the reentry maneuvering system of the
Pedro Luiz Kaled Da Cás, Cristiano Queiroz Vilanova, Manuel Nascimento Dias Barcelos Jr., Carlos Alberto Gurgel Veras   +3 more
doaj  

Beyond Accuracy: A Reliability-Oriented Multi-Dimensional Benchmark of Data-Driven Fault Diagnosis for Liquid Rocket Engines. [PDF]

Sensors (Basel)
Geng M, Zheng G, He L, Zhao S, Yu X.
europepmc   +1 more source

Preliminary design of a hybrid rocket engine

The aerospace industry has experienced significant growth in recent years, leading to increased demand for propulsion systems for launch vehicles aimed at placing satellites into orbit, space tourism, upper stages, lunar and planetary landing modules, among other applications. Alongside this growth, there has been a rising demand for propulsion systems
openaire   +1 more source

Bioconvection driven flow of magnetized micropolar hybrid nanofluid with Ohmic heating and variable thermal conductivity. [PDF]

Discov Nano
Saleem M, Haq F, Ghazwani HA, Areshi M, Younis J.   +4 more
europepmc   +1 more source

A hybrid RAG and rule-based reasoning framework for technical document analysis. [PDF]

Front Artif Intell
Thomas ER, Natarajan N, Jayaprakashan K, Malini A.   +3 more
europepmc   +1 more source

Multimatrix Composite Materials for Rocket Nozzle Manufacturing: A Comparative Review. [PDF]

Polymers (Basel)
Meiirbekov M, Sadykov M, Kuandyk A, Nurguzhin M, Janikeyev M, Gulmaira P, Mustafa L, Yesbolov N.   +7 more
europepmc   +1 more source

Hybrid rocket engine on the methane clathrate

Kosmìčna nauka ì tehnologìâ, 2017
A.S. Levenko, V.I. Prysiazhnyi, O.L. Pauk, A.S. Drozdenko   +3 more
openaire   +1 more source