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Design and Performance of an Electrowetting Ionic Liquid Electrospray Thruster Prototype
- Wei Sun,
- Yuntao Guo,
- Zhiwen Wu,
- Zening Du,
- Ningfei Wang and
- Zhenning Sun
30 November 2023Journal of Propulsion and Power Articles in Advance
https://doi.org/10.2514/1.B39201
Abstract
Abstract
Porous ionic liquid electrospray thrusters are capable of meeting the propulsion requirements of micro- and nanosatellites. The liquid propellant of such a thruster is usually prefilled in the porous reservoir and emitter, then passively and ...
No Access
Direct, Continuous Condensation of Steam in Flowing Water
- Jim A. Clark and
- Ryan W. Brandt
Oct.-Nov. 2005Journal of Thermophysics and Heat Transfer Volume 19, Issue 4
https://doi.org/10.2514/1.14033
- First Page
- Read Now
No Access
Optimal Relocation of Satellites Flying in Near-Circular-Orbit Formations
- Phil Palmer
May/June 2006Journal of Guidance, Control, and Dynamics Volume 29, Issue 3
https://doi.org/10.2514/1.14310
- First Page
- Read Now
No Access
Numerical Analysis of Free-Molecule Microresistojet Performance
July/Aug. 2006Journal of Propulsion and Power Volume 22, Issue 4
https://doi.org/10.2514/1.19570
- First Page
- Read Now
No Access
Free-Molecule-Microresistojet Performance Using Water Propellant for Nanosatellite Applications
- R. H. Lee ,
- A. M. Bauer ,
- M. D. Killingsworth ,
- T. C. Lilly ,
- J. A. Duncan and
- A. D. Ketsdever
Mar./Apr 2008Journal of Spacecraft and Rockets Volume 45, Issue 2
https://doi.org/10.2514/1.32341
- First Page
- Read Now
No Access
Ablative Impulse Characteristics of Polyacetal with Repetitive CO2 Laser Pulses
- Koji Suzuki ,
- Keisuke Sawada ,
- Ryota Takaya and
- Akihiro Sasoh
July/Aug. 2008Journal of Propulsion and Power Volume 24, Issue 4
https://doi.org/10.2514/1.32477
- First Page
- Read Now
No Access
Arcjet Plasma Neutralization of Hall Thrusters, Part 2: Experimental Demonstration
Nov./Dec. 2004Journal of Spacecraft and Rockets Volume 41, Issue 6
https://doi.org/10.2514/1.3280
- First Page
- Read Now
No Access
Influence of Electrode Shape on Performance of Pulsed Magnetoplasmadynamic Thruster SIMP-LEX
Mar/Apr 2009Journal of Propulsion and Power Volume 25, Issue 2
https://doi.org/10.2514/1.35568
- First Page
- Read Now
No Access
Microstructure Effects in Aluminized Solid Rocket Propellants
- L. T. DeLuca ,
- L. Galfetti ,
- G. Colombo ,
- F. Maggi ,
- A. Bandera ,
- V. A. Babuk and
- V. P. Sinditskii
Jul/Aug 2010Journal of Propulsion and Power Volume 26, Issue 4
https://doi.org/10.2514/1.45262
- First Page
- Read Now
No Access
Ionic Liquid Dual-Mode Spacecraft Propulsion Assessment
- Brian R. Donius and
- Joshua L. Rovey
Jan/Feb 2011Journal of Spacecraft and Rockets Volume 48, Issue 1
https://doi.org/10.2514/1.49959
- First Page
- Read Now
No Access
Fabrication and Operation of Microfabricated Emitters as Components for a Colloid Thruster
- John Stark ,
- Bob Stevens ,
- Matthew Alexander and
- Barry Kent
July/Aug. 2005Journal of Spacecraft and Rockets Volume 42, Issue 4
https://doi.org/10.2514/1.7537
- First Page
- Read Now
No Access
A Critical History of Electric Propulsion: The First 50 Years (1906-1956)
- E. Y. Choueiri
Mar./Apr. 2004Journal of Propulsion and Power Volume 20, Issue 2
https://doi.org/10.2514/1.9245
- First Page
- Read Now
No Access
Constant Momentum Exchange to Maintain Spacecraft Formations
- Jacob Schonig and
- Andrew Ketsdever
Jan/Feb 2012Journal of Spacecraft and Rockets Volume 49, Issue 1
https://doi.org/10.2514/1.A32017
- First Page
- Read Now
No Access
Responsiveness in Low Orbits Using Electric Propulsion
- Thomas C. Co and
- Jonathan T. Black
20 February 2014Journal of Spacecraft and Rockets Volume 51, Issue 3
https://doi.org/10.2514/1.A32405
Abstract
Abstract
One promising option for space operational responsiveness is orbital maneuvering. In low orbit, a maneuverable spacecraft can provide valuable benefits such as better coverage properties, reduced revisit times, selectable targets, and local overflight ...
No Access
Feasibility for Orbital Life Extension of a CubeSat in the Lower Thermosphere
28 June 2016Journal of Spacecraft and Rockets Volume 53, Issue 5
https://doi.org/10.2514/1.A33462
Abstract
Abstract
Orbital flight of CubeSats at altitudes between 150 and 250 km has the potential to enable a new class of scientific, commercial, and defense-related missions. A study is presented to demonstrate the feasibility of extending the orbital lifetime of a ...
No Access
Analytical Modeling of Heat Deposition in Propellant for Nuclear Thermal Rockets
27 March 2019Journal of Spacecraft and Rockets Volume 56, Issue 5
https://doi.org/10.2514/1.A34389
Abstract
Abstract
Nuclear thermal propulsion (NTP) is an enabling technology for expanding spaceflight capability beyond cislunar space. Hydrogen propellant is required for best efficiency by mass, but long-term hydrogen propellant storage is difficult as it must be stored ...
No Access
Autophage Engines: Method to Preset Gravity Load of Solid Rockets
2 January 2020Journal of Spacecraft and Rockets Volume 57, Issue 2
https://doi.org/10.2514/1.A34597
Abstract
Abstract
A retardation effect, which is the decrease of the feed pressure and the thrust of an autophage rocket, is considered. The effect is caused by inertial forces acting on the rocket sliding engine and has an exponential decay pattern. It is proposed to ...
No Access
Event-Driven Network Model for Space Mission Optimization with High-Thrust and Low-Thrust Spacecraft
- Bindu B. Jagannatha and
- Koki Ho
14 March 2020Journal of Spacecraft and Rockets Volume 57, Issue 3
https://doi.org/10.2514/1.A34628
Abstract
Abstract
Numerous high-thrust and low-thrust space propulsion technologies have been developed in the recent years with the goal of expanding space exploration capabilities; however, designing and optimizing a multimission campaign with both high-thrust and low-...
No Access
Extraction of Pendulum Model Parameters from Steady-State Slosh Data in Diaphragm Tanks
16 February 2022Journal of Spacecraft and Rockets Volume 59, Issue 3
https://doi.org/10.2514/1.A35146
Abstract
Abstract
This study proposes a new experimental approach to extract pendulum model parameters from spacecraft propellant tank slosh data. The novelty of the approach is in the utilization of steady-state triaxial force measurements at the support points of the ...
No Access
Strategic Forecasting Toward Achieving Defensible Space Architecture by Year 2030
25 May 2022Journal of Spacecraft and Rockets Volume 59, Issue 5
https://doi.org/10.2514/1.A35191
Abstract
Abstract
Along with the increased demand for space access transportation, a rise in adversarial offensive capabilities, and increasing reliance upon space-based assets, U.S. space assets are now more vulnerable to ground- and space-based threats than ever. The ...

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Design and Performance of an Electrowetting Ionic Liquid Electrospray Thruster Prototype

Abstract

Direct, Continuous Condensation of Steam in Flowing Water

Optimal Relocation of Satellites Flying in Near-Circular-Orbit Formations

Numerical Analysis of Free-Molecule Microresistojet Performance

Free-Molecule-Microresistojet Performance Using Water Propellant for Nanosatellite Applications

Ablative Impulse Characteristics of Polyacetal with Repetitive CO2 Laser Pulses

Arcjet Plasma Neutralization of Hall Thrusters, Part 2: Experimental Demonstration

Influence of Electrode Shape on Performance of Pulsed Magnetoplasmadynamic Thruster SIMP-LEX

Microstructure Effects in Aluminized Solid Rocket Propellants

Ionic Liquid Dual-Mode Spacecraft Propulsion Assessment

Fabrication and Operation of Microfabricated Emitters as Components for a Colloid Thruster

A Critical History of Electric Propulsion: The First 50 Years (1906-1956)

Constant Momentum Exchange to Maintain Spacecraft Formations

Responsiveness in Low Orbits Using Electric Propulsion

Abstract

Feasibility for Orbital Life Extension of a CubeSat in the Lower Thermosphere

Abstract

Analytical Modeling of Heat Deposition in Propellant for Nuclear Thermal Rockets

Abstract

Autophage Engines: Method to Preset Gravity Load of Solid Rockets

Abstract

Event-Driven Network Model for Space Mission Optimization with High-Thrust and Low-Thrust Spacecraft

Abstract

Extraction of Pendulum Model Parameters from Steady-State Slosh Data in Diaphragm Tanks

Abstract

Strategic Forecasting Toward Achieving Defensible Space Architecture by Year 2030

Abstract