People Background Check
Find People:

Eugene M Levin, Age 664744 Hamilton Rd, Hopkins, MN 55345

Get Report
Known as:
Eugene Michael Levin Yevgeniy M Levin Eugene M Levih Gene Levin
Related to:
Tam H Nguyen 40

Eugene Levin Phones & Addresses

4744 Hamilton Rd, Minnetonka, MN 55345 (952) 933-3796

Hopkins, MN

Las Vegas, NV

8209 30 1/2 St, Minneapolis, MN 55426 (952) 938-8138

Saint Louis Park, MN

Laramie, WY

Work

Company: Carlson brands enterprise - Minneapolis, MN Mar 2012 Position: Strategy and marketing consultant

Military

Company: U.S. Army Nov 2000 to Jun 2011 Rank: Captain

Education

School / High School: UNIVERSITY OF MINNESOTA- Minneapolis, MN 2011 Specialities: MBA in Marketing Strategy

Skills

Fluent in Russian

Mentions for Eugene M Levin

Career records & work history

Lawyers & Attorneys

Eugene Levin Photo 1

Eugene Levin - Lawyer

Specialties:
Federal Taxation Law, Corporate Transactions
ISLN:
905493433
Admitted:
1984
University:
University of Illinois, B.S., 1981
Law School:
IIT/Chicago-Kent College of Law, J.D., 1984; IIT/Chicago-Kent College of Law, LL.M., 1989
Eugene Levin Photo 2

Eugene Levin - Lawyer

Office:
Sony Music Entertainment
Specialties:
Licensing, Corporate & Incorporation, Contracts & Agreements
ISLN:
1000460992
Admitted:
2014
University:
New York University School of Law

Eugene Levin resumes & CV records

Resumes

Eugene Levin Photo 34

Founder

Location:
4744 Hamilton Rd, Minnetonka, MN 55345
Industry:
Aviation & Aerospace
Work:
Electrodynamic Technologies
Founder Aerospace Industry
Aerospace Contractor Institute For Mechanical Engineering Research 1983 - 1993
Senior Scientist
Education:
Lomonosov Moscow State University (Msu) 1974 - 1983
Doctorates, Doctor of Philosophy
Skills:
Aerospace, Spacecraft, Simulations, Propulsion, Astrodynamics, Orbital Mechanics
Eugene Levin Photo 35

Eugene Levin

Eugene Levin Photo 36

Full Time Mba Student Class Of 2013 At Carlson School Of Management

Location:
Greater Minneapolis-St. Paul Area
Industry:
Financial Services
Eugene Levin Photo 37

Eugene Levin - Burnsville, MN

Work:
CARLSON BRANDS ENTERPRISE - Minneapolis, MN Mar 2012 to May 2013
Strategy and Marketing Consultant CARLSON BRANDS ENTERPRISE - Minneapolis, MN Aug 2012 to Dec 2012
Social Media Marketing Intern CARLSON BRANDS ENTERPRISE - Minneapolis, MN May 2012 to Aug 2012
Summer Intern UNITED STATES ARMY Sep 2009 to Jun 2011
Intelligence Officer and Security Manager UNITED STATES ARMY Sep 2008 to Sep 2009
Intelligence Company Executive Officer UNITED STATES ARMY - El Paso, TX Nov 2000 to Jul 2007
Multiple Positions (Enlisted Soldier) Morgan Stanley - El Paso, TX Sep 2006 to Jan 2007
Financial Services Intern
Education:
UNIVERSITY OF MINNESOTA - Minneapolis, MN 2011 to 2013
MBA in Marketing Strategy THE UNIVERSITY OF TEXAS IN EL PASO - El Paso, TX May 2007
Bachelor of Business Administration in Finance
Military:
Rank: Captain Nov 2000 to Jun 2011
Branch: U.S. ArmyL.i.location.original
Skills:
Fluent in Russian

Publications & IP owners

Us Patents

Apparatus For Observing And Stabilizing Electrodynamic Tethers

US Patent:
6755377, Jun 29, 2004
Filed:
Dec 20, 2002
Appl. No.:
10/325224
Inventors:
Eugene M. Levin - Minnetonka MN
Joseph A. Carroll - Chula Vista CA
Assignee:
Tether Applications, Inc. - Chula Vista CA
International Classification:
B64G 100
US Classification:
244158R
Abstract:
A tether system for space applications includes at least one electron collector, at least one electron emitter, a power system, and at least one electrodynamic tether electrically coupled to the power system. The electrodynamic tether conducts electrical current between at least one electron collector and at least one electron emitter. Electric current and voltage are measured. Selected tether dynamics and electrodynamics based on the measured electric current and voltage are ascertained. The electric current and/or current distribution is adjusted to thereby control at least one tether system state based on the ascertained selected tether dynamics and electrodynamics.

Method For Observing And Stabilizing Electrodynamic Tethers

US Patent:
6758443, Jul 6, 2004
Filed:
Mar 7, 2002
Appl. No.:
10/094312
Inventors:
Eugene M. Levin - Minnetonka MN
Joseph A. Carroll - Chula Vista CA
Assignee:
Tether Applications, Inc. - Chula Vista CA
International Classification:
B64G 100
US Classification:
244158R
Abstract:
A tether system for space applications includes at least one electron collector, at least one electron emitter, a power system, and at least one electrodynamic tether electrically coupled to the power system. The electrodynamic tether conducts electrical current between at least one electron collector and at least one electron emitter. Electric current and voltage are measured. Selected tether dynamics and electrodynamics based on the measured electric current and voltage are ascertained. The electric current and/or current distribution is adjusted to thereby control at least one tether system state based on the ascertained selected tether dynamics and electrodynamics.

Method And Apparatus For Propulsion And Power Generation Using Spinning Electrodynamic Tethers

US Patent:
6942186, Sep 13, 2005
Filed:
Mar 5, 2002
Appl. No.:
10/092214
Inventors:
Eugene M. Levin - Minnetonka MN, US
Joseph A. Carroll - Chula Vista CA, US
Assignee:
Star Technology and Research, Inc. - Mount Pleasant SC
International Classification:
B64G001/32
US Classification:
244158R, 244172, 244166
Abstract:
The present invention improves the orbital maneuvering and power generation capabilities of a system of a satellite(s) connected with a conducting tether(s) by spinning the system about its mass center at an angular rate which is relatively high compared to the average orbital rate. An improvement in tether performance is achieved because at many times during rotation the tether is positioned at much better angles with the magnetic field and significantly higher currents are driven through the tether without destabilizing the system. The current can flow either in the direction of the EMF induced in the tether, or in the reverse direction, depending on the tether orientation with respect to the magnetic field and the mission goals. The reverse current is driven by the onboard power sources. Spinning electrodynamic tether systems can also be lighter and simpler in design and more flexible in operation.

Electrodynamic Structure

US Patent:
7913954, Mar 29, 2011
Filed:
Mar 10, 2006
Appl. No.:
11/372508
Inventors:
Eugene M. Levin - Minnetonka MN, US
Assignee:
Star Technology and Research, Inc. - Mount Pleasant SC
International Classification:
B64G 1/40
US Classification:
2441715
Abstract:
An electrodynamic structure having a periphery. The electrodynamic structure includes a power system, a plurality of collectors, a plurality of emitters, and conductive paths. The plurality of collectors are disposed on the periphery of the electrodynamic structure and configured to collect electrons. The plurality of emitters are disposed on the periphery of the electrodynamic structure and configured to emit electrons. At least 20% of the periphery of the electrodynamic structure is utilized for electron collection and electron emission. The conductive paths are configured to conduct current between the power system, the collectors, and the emitters to provide at least one of power generation and electrodynamic propulsion.

Electrodynamic Method

US Patent:
8262029, Sep 11, 2012
Filed:
Mar 9, 2011
Appl. No.:
13/044388
Inventors:
Eugene M. Levin - Minnetonka MN, US
Assignee:
Star Technology and Research, Inc. - Mount Pleasant SC
International Classification:
B64G 1/40
US Classification:
2441715
Abstract:
An electrodynamic method includes providing an electrodynamic structure with a periphery, providing power, collecting electrons, and emitting electrons. The emitting electrons and the collecting electrons utilizes at least 20% of the periphery of the electrodynamic structure. The method includes conducting current to provide at least one of electrodynamic propulsion and power generation.

In-Space Processing And Delivery System

US Patent:
2012029, Nov 22, 2012
Filed:
May 20, 2011
Appl. No.:
13/113001
Inventors:
Eugene M. Levin - Minnetonka MN, US
Joseph A. Carroll - Chula Vista CA, US
Jerome Pearson - Mount Pleasant SC, US
International Classification:
B64G 1/00
B64G 1/64
B64G 1/56
B64G 1/40
B64G 1/54
US Classification:
2441582, 2441711, 2441583
Abstract:
A processing and delivery system is in space around a celestial body having a magnetic field. The system includes at least one facility having supplies and configured for in-space recycling and manufacturing to produce processed objects utilizing space debris objects and the supplies. The system includes at least one space vehicle configured to deliver the space debris objects from their orbits to the at least one facility using electrodynamic propulsion. The system includes at least one space vehicle configured to deliver new supplies to the at least one facility from other orbits using electrodynamic propulsion. The system includes at least one space vehicle configured to deliver the processed objects from the at least one facility to their destination orbits using electrodynamic propulsion.

Separation System And Burn Wire Release Mechanism For Tethered Spacecraft

US Patent:
2015011, Apr 30, 2015
Filed:
Mar 29, 2014
Appl. No.:
14/229905
Inventors:
Shannon Coffey - Springfield VA, US
Joseph A. Carroll - Chula Vista CA, US
Paul Oppenheimer - Edgewater MD, US
Jordan R. Schlater - Rossburg OH, US
Ivan Galysh - Chantilly VA, US
Eugene Levin - Minnetonka MN, US
Curt Hogan - Napoleon OH, US
Adam Thurn - Washington DC, US
Assignee:
The Government of the US, as represented by the Secretary of the Navy - Washington DC
International Classification:
B64G 1/64
B64G 1/42
US Classification:
2441582
Abstract:
A tethered spacecraft has a first endmass and a second endmass with a telescoping stacer spring and a tether arranged between the endmasses. The spring is coiled around a center rod and initially contained within a housing, the spring being biased to push the first endmass away from the second endmass. The spring housing is affixed to the first endmass, a first end of the spring being affixed to the spring housing, and tether are affixed to spring at one end and to the second endmass at the other end. A pretensioned loop holds the endmasses abuttingly together, and a burnwire release mechanism cuts the loop to deploy the spring. Upon deployment, the spring extends to its full length to form a cylindrical boom, and the endmasses continue to move outward along the spring centerline until stopped by the tether.

Isbn (Books And Publications)

Dynamic Analysis Of Space Tether Missions

Author:
Eugene M. Levin
ISBN #:
0877035377

Possible Relatives

Cynthia E Levin  David A Levin  Daniel J Levin  Denise Levin  Danielle V Levin  Diana A Levin  Dmitry M Levin  Eugene F Johnston  Eugene C Stang  Eugene F White 

NOTICE: You may not use PeopleBackgroundCheck or the information it provides to make decisions about employment, credit, housing or any other purpose that would require Fair Credit Reporting Act (FCRA) compliance. PeopleBackgroundCheck is not a Consumer Reporting Agency (CRA) as defined by the FCRA and does not provide consumer reports.