Results 121 to 130 of about 1,790,414 (217)

A dynamic simulation approach to optimize thrust regulation in electric pump-fed rocket engines. [PDF]

Sci Rep
Li T, He H, Yu N, Sun X, Cai G.
europepmc   +1 more source

HYDRA III Hybrid Rocket Engine - Flight Version Test Results

, 2015
The flight version of the HYDRA III hybrid rocket engine was built by the ExperimentalRaumfahrt-InteressenGemeinschaft e.V. (ERIG) in cooperation with the Institute of Aerospace Systems of TU Braunschweig. The HYDRA III engine was improved to a thrust of
Hink, Rüdiger
core  

Design of an onboard computer for small experimental rockets with an integrated hardware-in-the-loop validation framework. [PDF]

HardwareX
Netzel NA, Rosa LG, Granziera F, Tosin MC, Batista DS.   +4 more
europepmc   +1 more source

Bayesian Convolutional Neural Networks for Uncertainty-Aware Classification of Infrasound Events. [PDF]

Sensors (Basel)
Yin H, Zhang K, Lu Y, Chang Y, Wu Y, Yang F, Li X, Xu J, Pang X.   +8 more
europepmc   +1 more source

Estimating CO2 emissions due to present and future suborbital space tourism industry. [PDF]

PLoS One
Huang AM, Xu Y.
europepmc   +1 more source

Physics-Topology-Anchored Learning: A Robust and Lightweight Framework for Time-Series Prediction and Anomaly Detection Under Data Scarcity. [PDF]

Sensors (Basel)
Hua X, Yin W, Wang L, Ma M, Yuan J, Zhang J.   +5 more
europepmc   +1 more source

Application of Gaussian SVM Flame Detection Model Based on Color and Gradient Features in Engine Test Plume Images. [PDF]

Sensors (Basel)
Yan S, Gao Y, Zhang Z, Li Y.
europepmc   +1 more source

Predictive maintenance programs for aircraft engines based on remaining useful life prediction. [PDF]

Sci Rep
Xue F, Jin G, Tan L, Zhang C, Yu Y.
europepmc   +1 more source

Development of an Optimized Induction Melting System for Fabricating Paraffin Fuel Grains for Hybrid Rocket Propulsion

Journal of Aerospace Technology and Management
This work reports the development of an induction melting system for producing paraffin-based fuel units for hybrid rockets. The system is based in oscillating low-frequency magnetic field to generate heat within the material, enabling a precise ...
José Refugio Martínez, José Ángel de la Cruz-Mendoza, Emmanuel Vázquez-Martínez, Daniel Romero de la Cruz, Azdrubal Lobo Guerrero, Gerardo Saucedo-Zárate, José Luis Arauz-Lara, Hernán González-Aguilar, Gerardo Ortega-Zarzosa   +8 more
doaj  

Analysis of carbon nano particle variant as the propellant fuel to increase specific impulses of rockets. [PDF]

F1000Res, 2023
Navalino R, Muda N, Hafizah M, Ruyat Y.
europepmc   +1 more source