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Thrusters (spacecraft)

  • An Assessment of Aerocapture and Applications to Future Missions

    An Assessment of Aerocapture and Applications to Future Missions

  • Gravity-Assist Trajectories to Jupiter Using Nuclear Electric Propulsion

    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

    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

    1 Iac-06-C4.4.7 the Innovative Dual-Stage 4-Grid Ion

  • Single-Stage Drag Modulation GNC Performance for Venus Aerocapture Demonstration

    Single-Stage Drag Modulation GNC Performance for Venus Aerocapture Demonstration

  • Space Propulsion Technology for Small Spacecraft

    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

    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

    In-Space Propulsion Data Sheets

  • Simulation and Study of Gravity Assist Maneuvers

    Simulation and Study of Gravity Assist Maneuvers

  • Future Directions for Electric Propulsion Research

    Future Directions for Electric Propulsion Research

  • Movement and Maneuver in Deep Space: a Framework to Leverage Advanced Propulsion

    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

    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

    Optimization of Low-Thrust Gravity Assist Trajectories Under Application of Tisserand’S Criterion

  • Small Satellite Aerocapture for Increased Mass Delivered to Venus and Beyond

    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

    Using Gravity Assist Maneuver to Increase Fuel Consumption Efficiency for a Space Probe Entering Jupiter’S Orbit

  • Thruster Principles

    Thruster Principles

  • Capability of Solar Electric Propulsion for Planetary Missions Giuseppe D

    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

    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


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