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Rocket Propulsion in Gravitational Field - II01:03

Rocket Propulsion in Gravitational Field - II

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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...
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Rocket Propulsion in Gravitational Field - I01:20

Rocket Propulsion in Gravitational Field - I

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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...
2.8K
Rocket Propulsion in Empty Space - I01:13

Rocket Propulsion in Empty Space - I

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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...
3.2K
Rocket Propulsion In Empty Space - II01:12

Rocket Propulsion In Empty Space - II

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The motion of a rocket is governed by the conservation of momentum principle. A rocket's momentum changes by the same amount (with the opposite sign) as the ejected gases. As time goes by, the rocket's mass (which includes the mass of the remaining fuel) continuously decreases, and its velocity increases. Therefore, the principle of conservation of momentum is used to explain the dynamics of a rocket's motion. The ideal rocket equation gives the change in velocity that a rocket...
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PD Controller: Design01:26

PD Controller: Design

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In automotive engineering, car suspension systems often employ Proportional Derivative (PD) controllers to enhance performance. PD controllers are utilized to adjust the damping force in response to road conditions. A controller, acting as an amplifier with a constant gain, demonstrates proportional control, with output directly mirroring input.
Designing a continuous-data controller requires selecting and linking components like adders and integrators, which are fundamental in Proportional,...
208
Torque Free Motion01:15

Torque Free Motion

467
The torque-free motion refers to the movement of a rigid body in space when no external torques are acting upon it. This type of motion can be observed in environments where there are no external forces or frictions, like in outer space. For example, a rotation of Mars in space is a torque-free motion. Mars is an axisymmetric object, meaning it has an axis of symmetry along which it rotates, designated as the z-axis. The rotating frame of reference is defined such that the center of mass of...
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Related Experiment Video

Updated: Jun 17, 2025

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

Optimization, Test and Diagnostics of Miniaturized Hall Thrusters

Published on: February 16, 2019

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Lab-on-PCB solid propellant microthruster with multi-mode thrust capabilities.

Jeongrak Lee1, Seonghyeon Kim1, Hanseong Jo1

  • 1Department of Mechanical Engineering, Pohang University of Science and Technology, Pohang, Gyeongbuk 37673, Republic of Korea. annalee@postech.ac.kr.

Lab on a Chip
|August 7, 2024
PubMed
Summary
This summary is machine-generated.

A novel shared-chamber solid-propellant microthruster, built using lab-on-printed-circuit-board (PCB) technology, offers consistent thrust and multiple modes for nano/microsatellite applications.

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Area of Science:

  • Aerospace Engineering
  • Materials Science
  • Nanotechnology

Background:

  • Growing demand for microthrusters in nano/microsatellite clustering.
  • Existing solid propellant microthrusters face challenges in thrust consistency, scalability, and durability.
  • Limitations of traditional MEMS-based microthruster fabrication.

Purpose of the Study:

  • To propose and develop a novel shared-chamber solid-propellant microthruster design.
  • To address issues of inconsistent thrust, limited modes, and production challenges.
  • To leverage lab-on-printed-circuit-board (PCB) technology for enhanced microthruster fabrication.

Main Methods:

  • Design and fabrication of a shared-chamber microthruster using lab-on-PCB and PCB surface mount technology.
  • Implementation of ignition and combustion experiments to verify unit operation.
  • Evaluation of different operational modes, including power and continuous thrust.

Main Results:

  • Consistent thrust generation at a designated position.
  • Successful accommodation of multiple thrust modes (power and continuous).
  • Demonstrated enhanced structural stability, scalability, and potential for mass production via PCB technology.

Conclusions:

  • The lab-on-PCB-based shared-chamber solid propellant microthruster offers a viable solution for satellite propulsion.
  • The design overcomes limitations of existing microthrusters, providing improved performance and manufacturability.
  • Integration with propulsion and electronic control systems shows significant potential for future satellite missions.