Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Russell A. Lawton"'
Autor:
Dean V. Wiberg, Thomas R. VanZandt, Russell A. Lawton, Gisela Lin, Judith A. Podosek, T. George, Allan P. Hui, Victor White, Indrani Chakraborty, Joanne Wellman, Kirill Shcheglov, Colleen M. Marrese, Juergen Mueller, Stephen Vargo, Christopher Evans, Sam Young Bae, Eui-Hyeok Yang, Tony Tang, Beverley Eyre, Kevin King, Amanda A. Green, H. Lynn Kim, Hillary Cherry
Publikováno v:
SPIE Proceedings.
The MEMS Technology Group is part of the Microdevices Laboratory (MDL) at the Jet Propulsion Laboratory (JPL). The group pursues the development of a wide range of advanced MEMS technologies that are primarily applicable to NASA's robotic as well as
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::70af805f8e2326c270eb1959c061e3e8
https://doi.org/10.1117/12.405340
https://doi.org/10.1117/12.405340
Publikováno v:
SPIE Proceedings.
A study to evaluate three processes used for the release of standard devices produced by MCNC using the MUMPS process was undertaken by Jet Propulsion Laboratory with the collaboration of The Aerospace Corporation, and Polytec PI. The processes used
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0bf9f2d603ad0fbfce26fb643d37d927
https://doi.org/10.1117/12.359370
https://doi.org/10.1117/12.359370
Autor:
David Pyle, William C. Tang, Russell A. Lawton, Indrani Chakraborty, Juergen Mueller, Ronald Ruiz
Publikováno v:
Scopus-Elsevier
Low-temperature (LTO) chemical vapor deposited (CVD) silicon dioxide was investigated for use as an insulator material in microfabricated ion engine accelerator grids. Both substrate (bulk) as well as surface breakdown experiments were performed. Oxi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f1fbdc5e32fab01baf78ffa9150e1c0d
https://doi.org/10.2514/6.1998-3923
https://doi.org/10.2514/6.1998-3923
Autor:
Juergen Mueller, Andrew P. Wallace, Indrani Chakraborty, Russell A. Lawton, David Bame, William C. Tang
Publikováno v:
Scopus-Elsevier
Proof-of-concept testing of a microfabricated vaporizing liquid thruster was performed. In this liquid-fed thruster concept, propellant vaporization is achieved in a microfabricated thin film heater arrangement. Chip temperatures of 100, 150 and 200
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f7e2a856b932676b0d45a843d02ec8c7
http://www.scopus.com/inward/record.url?eid=2-s2.0-84963860880&partnerID=MN8TOARS
http://www.scopus.com/inward/record.url?eid=2-s2.0-84963860880&partnerID=MN8TOARS
