Propulsion for cubesats

K Lemmer - Acta Astronautica, 2017 - Elsevier
At present, very few CubeSats have flown in space featuring propulsion systems. Of those
that have, the literature is scattered, published in a variety of formats (conference …

Capillary ionic liquid electrospray: beam compositional analysis by orthogonal time-of-flight mass spectrometry

SW Miller, JR Ulibarri-Sanchez, BD Prince… - Journal of Fluid …, 2021 - cambridge.org
Orthogonal time-of-flight mass spectrometry has been used to characterize the kinetic
energy and charged species distributions from an in vacuo electrospray ion source for four …

Magnetic (electric) drop deformation in uniform external fields: Volume averaged methods and formation of static and dynamic conical tips

K Misra - Physics of Fluids, 2020 - pubs.aip.org
Analytical relationships describing droplet deformation in external magnetic (electric) fields
rely on spheroidal and ellipsoidal shape approximations. We show that the ellipsoidal shape …

[HTML][HTML] Orthogonal time-of-flight mass spectrometry of an ion beam with a broad kinetic energy profile

SW Miller, BD Prince, RJ Bemish - Review of Scientific Instruments, 2017 - pubs.aip.org
A combined experimental and modeling effort is undertaken to assess a detection system
composed of an orthogonal extraction time-of-flight (TOF) mass spectrometer coupled to a …

Mass spectrometry of selected ionic liquids in capillary electrospray at nanoliter volumetric flow rates

SW Miller, BD Prince, RJ Bemish… - 52nd AIAA/SAE/ASEE Joint …, 2016 - arc.aiaa.org
LECTROSPRAY thrusters constitute a class of micro-electric propulsion systems that use an
electric field to evaporate and accelerate an ionic propellant to generate thrust. This class of …

The effects of magnetic surface stress on electrospray of an ionic liquid ferrofluid

KJ Terhune, LB King, BD Prince, N Jain… - 52nd AIAA/SAE/ASEE …, 2016 - arc.aiaa.org
PPLYING a strong electrostatic stress to the interface of a conductive or dielectric liquid
creates an instability in the surface. If the stress is sufficiently large to balance the …

[PDF][PDF] Time Resolved Divergence Mapping and Long Duration Emission Studies of an Ionic Liquid Ferrofluid Electrospray Source

BA Jackson, LB King - 35th International Electric Propulsion …, 2017 - aerospace.mtu.edu
The electrospray emission of a super-paramagnetic fluid in the presence of a strong
magnetic field is investigated herein. Magnetic particles within the spray fluid experience a …

Verification of a Novel Electrospray Thruster with Magnetic Ionic liquid Propellant

Y Yuntian, L Xiaokang, G Dawei… - 2021 12th International …, 2021 - ieeexplore.ieee.org
A new concept of magnetic ionic liquid electrospray thruster (ILET) is proposed in this paper.
The thruster uses a lower working voltage with the action of an applied magnetic field, and is …

[PDF][PDF] AFRL-AFOSR-VA-TR-2018-0359

M UNI, V TY - academia.edu
The performance of a single tip ionic liquid ferrofluid electrospray source was estimated. The
electrospray source was sprayed until the fluid reservoir was depleted (typically 15 to 18 …

Derived Performance Metrics and Angular Efficiency of an Ionic Liquid Ferrofluid Electrospray Propulsion Concept

B Jackson, KJ Terhune, LB King - 2018 Joint propulsion conference, 2018 - arc.aiaa.org
The performance of a single tip ionic liquid ferrofluid electrospray source was estimated. The
electrospray source was sprayed until the fluid reservoir was depleted (typically 15 to 18 …