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Steven C Sara

from South Jordan, UT
Age ~68
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Also known as:
Steven Living Sara, Steven G Sara, Steve C Sara, Daniel Steven Sara, Sara Steven
Phone and address:
3052 Memorial Cir, Riverton, UT 84095
(801) 253-3905
Related to:
Donovan Platt, 46J SaraMark J Sanderson, 44Emily Sara, 41J Sara, 65Jan P Sara, 65Darla F Stevenson, 55Brandon D Sara, 36Sharlee Sara, 36
Connected to:
Albert G Sara, 42Heather M Sara, 50Jason J Sara, 66Jay R Sara, 82Laurence M Sara, 76Marsha R Sara, 75Miguel F Sara, 28Pamela P Sara, 76Sharon L Sara, 70Shirley R Sara, 90

Steven Sara Phones & Addresses

  • 3052 Memorial Cir, South Jordan, UT 84095 (801) 253-3905
  • Mantua, UT

Professional Records

Medicine Doctors

Steven Sara Photo 1

Steven Sara

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Specialties:
Anesthesiology
Work:
Metropolitan Anesthesiology
6501 Coyle Ave, Carmichael, CA 95608
(916) 966-6544 (phone), (916) 966-6547 (fax)

Metropolitan Anesthesiology
5530 Birdcage St STE 145, Citrus Heights, CA 95610
(916) 966-6544 (phone), (916) 966-6547 (fax)
Education:
Medical School
University of Nevada School of Medicine
Graduated: 2008
Languages:
English
Spanish
Description:
Dr. Sara graduated from the University of Nevada School of Medicine in 2008. He works in Carmichael, CA and 1 other location and specializes in Anesthesiology. Dr. Sara is affiliated with Mercy San Juan Medical Center.
Steven Sara Photo 2

Steven John Sara

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Specialties:
Anesthesiology
Surgery
Education:
University of Nevada (2008)

Publications

Us Patents

Non-Circular Cross-Section Missile Components, Missiles Incorporating Same, And Methods Of Operation

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US Patent:
20100242772, Sep 30, 2010
Filed:
Mar 24, 2009
Appl. No.:
12/410283
Inventors:
Phillip R. Martineau - Salt Lake City UT, US
Christopher J. Sullivan - Sandy UT, US
David W. Hull - Magna UT, US
Steven C. Sara - South Jordan UT, US
International Classification:
F42B 15/10
B64F 1/04
US Classification:
102380, 102374, 244 63
Abstract:
A missile component such as a rocket motor case, of an initial transverse cross-sectional shape flexible into another, different cross-section responsive to application of internal pressure from ignition of a propellant grain within the component. A missile launch assembly including at least one missile of a non-circular cross-section disposed within a segment of a partitioned circular launch tube. A multi-stage missile comprising at least a first stage and a second stage having rocket motor cases of non-circular transverse cross-section, the rocket motor case of at least one of the stages being deformable into another, different cross-section. A method of launching a missile including igniting a rocket motor of a component having a first cross-section, internally pressurizing the missile component substantially concurrently with motor ignition and flexing the component rocket motor into a second, different cross-sectional shape.
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Steven C Sara from South Jordan, UT, age ~68 Get Report