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Thrusters (spacecraft)
An Assessment of Aerocapture and Applications to Future Missions
Gravity-Assist Trajectories to Jupiter Using Nuclear Electric Propulsion
Study of a Crew Transfer Vehicle Using Aerocapture for Cycler Based Exploration of Mars by Larissa Balestrero Machado a Thesis S
1 Iac-06-C4.4.7 the Innovative Dual-Stage 4-Grid Ion
Single-Stage Drag Modulation GNC Performance for Venus Aerocapture Demonstration
Space Propulsion Technology for Small Spacecraft
The Spacedrive Project – First Results on Emdrive and Mach-Effect Thrusters BARCELO RENACIMIENTO HOTEL, SEVILLE, SPAIN / 14 – 18 MAY 2018
In-Space Propulsion Data Sheets
Simulation and Study of Gravity Assist Maneuvers
Future Directions for Electric Propulsion Research
Movement and Maneuver in Deep Space: a Framework to Leverage Advanced Propulsion
Investigation of Propellant Sloshing and Zero Gravity Equilibrium for the Orion Service Module Propellant Tanks
Optimization of Low-Thrust Gravity Assist Trajectories Under Application of Tisserand’S Criterion
Small Satellite Aerocapture for Increased Mass Delivered to Venus and Beyond
Using Gravity Assist Maneuver to Increase Fuel Consumption Efficiency for a Space Probe Entering Jupiter’S Orbit
Thruster Principles
Capability of Solar Electric Propulsion for Planetary Missions Giuseppe D
Hydrazine Thrusters and Propulsion Systems for Horse’ Thrusters with the Benefit of a Consistent Production Commercial, Scientific and Military Spacecraft
Top View
On a New Type of Combined Solar–Thermal/Cold Gas Propulsion System Used for LEO Satellite’S Attitude Control
An Overview of Cube-Satellite Propulsion Technologies and Trends
Plasma, Ion-Thrusters, and VASIMR
On the Exhaust of Electromagnetic Drive Patrick Grahn, Arto Annila, and Erkki Kolehmainen
HIGH-POWER SOLAR ELECTRIC PROPULSION in SPACE Joshua P
Commercial Spaceflight and Advanced Propulsion
Modern In-Space Electric Propulsion
Aerocapture Summary and Risk Discussion
Electric Propulsion and Plasma Dynamics Laboratory
Mars Aerocapture Systems Study
Pulsed Plasma Thruster Technology for Small Satellite Missions
Aerocapture Guidance Algorithm Development and Testing
4.3.1 Space Vehicle Control Systems
The 3D Fluid Simulations of the Solar Wind Interaction with Mars
Analysis About Constraints for Low-Thrust Gravity-Assist Sequencing
Design and Thermal Analysis of a Solar Thermal Thruster
Electric Propulsion
Design and Performance Analysis Study of an Ion Thruster
26N 2010 NASA NIAC NASA Institute for Advanced Concepts All Funded
4.2.1 Rockets and Launch Vehicles
Science Vs Science Fiction
Hall Thruster System Design for High Delta-V Missions 高ΔVミッションのためのホールスラスタシステム
Design and Optimization of Low-Thrust Gravity-Assist Trajectories to Selected Planets
Field Emission Electric Propulsion: Experimental Investigations on Microthrust FEEP Thrusters
Liquid-Fed Pulsed Plasma Thruster for Propelling Nanosatellites Adam R
Electric Propulsion Methods for Small Satellites: a Review
Responding to Mechanical Antigravity
Performance Characteristics Design of Pulsed Plasma Thrusters for Drag Counter-Reacting
Electric Propulsion
Spacecraft Propulsion, Launch and Orbit Design Rocket Scientists Gift to Exoplanet Scientists
Pulsed Plasma Thrusters: a Worldwide Review and Long Yearned Classification
Hypothetical Gravity Control and Possible Influence on Space Propulsion
Advantages of a Continuous Thrust Strategy from a Geosynchronous Transfer Orbit, Using High Specific Impulse Thrusters
POLITECNICO DI TORINO Analysis of Electric Propulsion Transfers For
A Novel Method for Low-Thrust Gravity-Assist Trajectory Optimization
Chemical and Plasma Rocket Propulsion
Oidtsaki Type: IQP Date: 5/2007 Project Number: JMW-NIAC