Micropropulsion devices with pulsed optical lattices / gas nonresonant dipole interaction

Mikhail N. Shneider, Cedrick Ngalande, Sergey F. Gimelshein

Research output: Chapter in Book/Report/Conference proceedingConference contribution

2 Scopus citations

Abstract

The direct simulation Monte Carlo method is used to study the feasibility of new propulsion concepts based on the interaction of an optical lattice with gas molecules. Two regimes are considered, high density and low density. In the first one, a de Lavai nozzle is examined with the carrier gas driven by energy and momentum deposition from the lattice to the region near the nozzle throat. Analytical expressions are developed and compared with the numerical predictions, that describe the energy and momentum energy transfer between the lattice and the gas. In the second regime, a multiple orifice flow is considered with molecules accelerated to high velocities by a chirped lattice potential. Specific impulse of about 500 is obtained with the total thrust of over 10 μN per single 100 μm orifice.

Original languageEnglish (US)
Title of host publicationCollection of Technical Papers - 44th AIAA Aerospace Sciences Meeting
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
Pages9290-9301
Number of pages12
ISBN (Print)1563478072, 9781563478079
DOIs
StatePublished - 2006
Event44th AIAA Aerospace Sciences Meeting 2006 - Reno, NV, United States
Duration: Jan 9 2006Jan 12 2006

Publication series

NameCollection of Technical Papers - 44th AIAA Aerospace Sciences Meeting
Volume13

Other

Other44th AIAA Aerospace Sciences Meeting 2006
Country/TerritoryUnited States
CityReno, NV
Period1/9/061/12/06

All Science Journal Classification (ASJC) codes

  • Space and Planetary Science
  • Aerospace Engineering

Fingerprint

Dive into the research topics of 'Micropropulsion devices with pulsed optical lattices / gas nonresonant dipole interaction'. Together they form a unique fingerprint.

Cite this