Results 121 to 130 of about 1,081 (308)
Preliminary Design of a Laboratory Cylindrical Hall-Effect Thruster
A 3-cm cylindrical Hall thruster with permanent magnets was designed and modeled. The goal was to design a Hall thruster for Cal Poly’s propulsion laboratory of similar size and performance as Cal Poly’s MiXI thruster.
McGrail, Scott, Parker, Sam
core
ABSTRACT This study examines how environmental regulations can drive technological change, drawing on the innovation systems perspective and the strong Porter hypothesis (SPH). The SPH suggests that well‐designed stringent regulations can foster innovation and enhance firm competitiveness, performance, and survival, yet prior research remains largely ...
Muhammad Zubair Khan +3 more
wiley +1 more source
Multi-Sensor Fault Diagnosis of Underwater Thruster Propeller Based on Deep Learning. [PDF]
Tsai CM +4 more
europepmc +1 more source
Performance Characteristics of Turkey’s First 1,5 kW Hall Thruster Electric Propulsion System
Due to significant advantages and successful applications, electric propulsion has become a key technology for both scientific and commercial space missions.
Demet Ulusen +7 more
doaj
ABSTRACT Environmental performance has become strategically critical as regulators mandate disclosure, investors screen for ESG commitments, and consumers reward sustainable practices. Yet whether environmental performance enhances or constrains corporate innovation capacity remains contested.
Jiyeon Kim, Wooyoung Yang
wiley +1 more source
Magnetic nozzle radiofrequency plasma thruster approaching twenty percent thruster efficiency. [PDF]
Takahashi K.
europepmc +1 more source
4.5-kW Hall Effect Thruster Evaluated
As part of an Interagency Agreement with the Air Force Research Lab (AFRL), a space simulation test of a Russian SPT 140 Hall Effect Thruster was completed in September 1999 at Vacuum Facility 6 at the NASA Glenn Research Center at Lewis Field.
Mason, Lee S.
core
Measurements of Plasma Potential Distribution in Segmented Electrode Hall Thruster [PDF]
Use of a segmented electrode placed at the Hall thruster exit can substantially reduce the voltage potential drop in the fringing magnetic field outside the thruster channel.
Fisch, N. J., Raitses, Y., Staack, D.
core
Development of KM-5 Hall effect thruster and its flight testing onboard GEO spacecraft “Express-A4”
The paper presents the outcomes of development of Keldysh Research Center (KeRC) KM-5 Hall effect thruster and experience obtained from the in-orbit exploiting of the thruster onboard Reshetnev's Scientific and Production Association of Applied Mechanics
A. A. Sinitsin +11 more
core +1 more source
Helicity-Aware Design of Hall-Type MHD Thrusters
We study thrust production in a single-fluid magnetohydrodynamic (MHD) thruster with Hall-type coaxial geometry and show how velocity–field alignment and magnetic topology set the operating regime.
Mario J. Pinheiro
doaj +1 more source

