Jove
Visualize
Contact Us

Related Concept Videos

Circular Orbits and Critical Velocity for Satellites01:16

Circular Orbits and Critical Velocity for Satellites

3.1K
The Moon orbits around the Earth. In turn, the Earth (and other planets) orbit the Sun. The space directly above our atmosphere is filled with artificial satellites in orbit. One can examine the circular orbit, the simplest kind of orbit, to understand the relationship between the speed and the period of planets and satellites with respect to their positions and the bodies that they orbit.
Nicolaus Copernicus (1473-1543) first suggested that the Earth and all other planets orbit the Sun in...
3.1K
Energy of a Satellite in a Circular Orbit01:11

Energy of a Satellite in a Circular Orbit

2.5K
Thousands of artificial satellites orbit the Earth every day at various distances from the Earth. Satellites that orbit the Earth below an altitude of 1,600 km are considered to be orbiting in low-Earth orbit (LEO). Research satellites and Earth observation satellites are usually placed in LEO, and mostly orbit the Earth in elliptical orbits. Navigation satellites are placed in medium-Earth orbit (MEO), ranging from 2,000 km to 36,000 km from the surface of the Earth. Meanwhile, communication...
2.5K
Rocket Propulsion in Gravitational Field - II01:03

Rocket Propulsion in Gravitational Field - II

2.5K
A rocket's velocity in the presence of a gravitational field is decreased by the amount of force exerted by Earth's gravitational field, which opposes the motion of the rocket. If we consider thrust, that is, the force exerted on a rocket by the exhaust gases, then a rocket's thrust is greater in outer space than in the atmosphere or on a launch pad. In fact, gases are easier to expel in a vacuum.
A rocket's acceleration depends on three major factors, consistent with the...
2.5K
Rocket Propulsion in Gravitational Field - I01:20

Rocket Propulsion in Gravitational Field - I

3.0K
Rockets range in size from small fireworks that ordinary people use to the enormous Saturn V that once propelled massive payloads toward the Moon. The propulsion of all rockets, jet engines, deflating balloons, and even squids and octopuses are explained by the same physical principle: Newton's third law of motion. The matter is forcefully ejected from a system, producing an equal and opposite reaction on what remains.
The motion of a rocket in space changes its velocity (and hence its...
3.0K
Rocket Propulsion in Empty Space - I01:13

Rocket Propulsion in Empty Space - I

3.4K
The driving force for the motion of any vehicle is friction, but in the case of rocket propulsion in space, the friction force is not present. The motion of a rocket changes its velocity (and hence its momentum) by ejecting burned fuel gases, thus causing it to accelerate in the direction opposite to the velocity of the ejected fuel. In this situation, the mass and velocity of the rocket constantly change along with the total mass of ejected gases. Due to conservation of momentum, the...
3.4K
Energy Stored In A Coaxial Cable01:31

Energy Stored In A Coaxial Cable

1.7K
A coaxial cable consists of a central copper conductor used for transmitting signals, followed by an insulator shield, a metallic braided mesh that prevents signal interference, and a plastic layer that encases the entire assembly.
In the simplest form, a coaxial cable can be represented by two long hollow concentric cylinders in which the current flows in opposite directions. The magnetic field inside and outside the coaxial cable is determined by using Ampère's law. The magnetic...
1.7K

You might also read

Related Articles

Articles linked to this work by shared authors, journal, and citation graph.

Sort by
Same author

A Multimodal Approach for Deep-Learning Classification of Vocal Fold Pathologies in Stroboscopy.

The Laryngoscope·2026
Same author

Autogenetic Gravity Center Placement.

Sensors (Basel, Switzerland)·2025
Same author

Bio-Inspired Space Robotic Control Compared to Alternatives.

Biomimetics (Basel, Switzerland)·2024
Same author

Space Robot Sensor Noise Amelioration Using Trajectory Shaping.

Sensors (Basel, Switzerland)·2024
Same author

Trust in Machine Learning Driven Clinical Decision Support Tools Among Otolaryngologists.

The Laryngoscope·2024
Same author

Bilinear Interpolation of Three-Dimensional Gain-Scheduled Autopilots.

Sensors (Basel, Switzerland)·2024
JoVE
x logofacebook logolinkedin logoyoutube logo
ABOUT JoVE
OverviewLeadershipBlogJoVE Help Center
AUTHORS
Publishing ProcessEditorial BoardScope & PoliciesPeer ReviewFAQSubmit
LIBRARIANS
TestimonialsSubscriptionsAccessResourcesLibrary Advisory BoardFAQ
RESEARCH
JoVE JournalMethods CollectionsJoVE Encyclopedia of ExperimentsArchive
EDUCATION
JoVE CoreJoVE BusinessJoVE Science EducationJoVE Lab ManualFaculty Resource CenterFaculty Site
Terms & Conditions of Use
Privacy Policy
Policies

Related Experiment Video

Updated: Oct 22, 2025

Optimization, Test and Diagnostics of Miniaturized Hall Thrusters
12:22

Optimization, Test and Diagnostics of Miniaturized Hall Thrusters

Published on: February 16, 2019

9.2K

Micro Satellite Orbital Boost by Electrodynamic Tethers.

Peter Yao1, Timothy Sands1

  • 1Sibley School of Mechanical and Aerospace Engineering, Cornell University, Ithaca, NY 14850, USA.

Micromachines
|August 27, 2021
PubMed
Summary

Electrodynamic tethers enable spacecraft to maintain orbit indefinitely by interacting with Earth's magnetic field, eliminating propellant constraints. This method is efficient for low Earth orbits but requires high power and is less effective for high inclination trajectories.

Keywords:
actuatorsaerodynamic dragand controlcubesatsdynamicsguidancemagnetic fieldmini/micro satellitesnavigationorbital dynamicsspacecraft maneuveringtether

More Related Videos

Thermocapillary Convection Space Experiment on the SJ-10 Recoverable Satellite
07:00

Thermocapillary Convection Space Experiment on the SJ-10 Recoverable Satellite

Published on: March 11, 2020

7.6K
A 100 KW Class Applied-field Magnetoplasmadynamic Thruster
11:47

A 100 KW Class Applied-field Magnetoplasmadynamic Thruster

Published on: December 22, 2018

9.3K

Related Experiment Videos

Last Updated: Oct 22, 2025

Optimization, Test and Diagnostics of Miniaturized Hall Thrusters
12:22

Optimization, Test and Diagnostics of Miniaturized Hall Thrusters

Published on: February 16, 2019

9.2K
Thermocapillary Convection Space Experiment on the SJ-10 Recoverable Satellite
07:00

Thermocapillary Convection Space Experiment on the SJ-10 Recoverable Satellite

Published on: March 11, 2020

7.6K
A 100 KW Class Applied-field Magnetoplasmadynamic Thruster
11:47

A 100 KW Class Applied-field Magnetoplasmadynamic Thruster

Published on: December 22, 2018

9.3K

Area of Science:

  • Spacecraft propulsion
  • Orbital mechanics
  • Electrodynamics

Background:

  • Traditional spacecraft propulsion relies on limited propellant, restricting mission duration and orbital maneuvers.
  • Maintaining long-term orbits, especially in low Earth orbit (LEO), faces challenges like atmospheric drag and orbital decay.
  • Electrodynamic tethers offer a propellantless alternative for spacecraft maneuvering and orbit maintenance.

Purpose of the Study:

  • To investigate the feasibility of using electrically charged tethers for indefinite spacecraft orbit maintenance in LEO.
  • To analyze the effects of Lorentz force and torque on spacecraft translational motion using tether systems.
  • To evaluate the efficiency and power requirements of electrodynamic tether propulsion for orbit boosting.

Main Methods:

  • Simulating spacecraft-tether system dynamics in LEO.
  • Applying Lorentz force and torque principles to Newton's translational motion and Euler's moment equations.
  • Analyzing the nonlinear coupling of six differential equations of motion for the system.

Main Results:

  • A 100-kg spacecraft with a 500-m tether and 1-amp current can gain 250 m in altitude per orbit.
  • Indefinite orbit maintenance at altitudes as low as 275 km is achievable by managing Lorentz forces and torques.
  • The electrodynamic tether system can counteract aerodynamic drag and maintain orbit height in very LEO.

Conclusions:

  • Electrodynamic tethers provide a viable, propellantless method for indefinite orbit maintenance in very low Earth orbits.
  • The reboost maneuver's efficiency is reduced for high inclination orbits, and it demands significant electrical power.
  • Higher power draw and longer tethers are necessary to counteract increased aerodynamic drag at lower altitudes.