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Frank A Sciorelli

from El Dorado Hills, CA
Age ~62
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Also known as:
Francesco Arturo Sciorelli, Francesco A Sciorelli, Frank I, Frank L
Phone and address:
4158 Monte Verde Dr, Folsom, CA 95762
Related to:
Janet Lynne Haynes, 64Taiwan Walker, 53Carmen Tamayo, 72James H Black, 71Rhonda Jackson, 77Ronald Haynes, 64
Connected to:
Kimberly J Sciorillo, 54Mario A Sciorrotta, 43Cosimo J Sciortino, 70Grace Sciortino, 88Guy J Sciortino, 73Julian Sciortino, 33Kay L Sciortino, 82Lauren L Sciortino, 39Lia M Sciortino, 42Louis P Sciortino, 63

Frank Sciorelli Phones & Addresses

  • 4158 Monte Verde Dr, El Dorado Hls, CA 95762
  • 567 Given St, Folsom, CA 95630
  • 635 Flower Dr, Folsom, CA 95630 (916) 983-3801
  • El Dorado Hills, CA
  • 6175 Bridgeport Dr, Shingle Spgs, CA 95682 (530) 672-6204
  • Shingle Springs, CA

Work

Company: Aerojet rocketdyne Oct 1987 Position: Principle product and chief engineer

Education

Degree: Bachelors, Bachelor of Science School / High School: California Polytechnic State University - San Luis Obispo 1981 to 1985 Specialities: Mechanical Engineering

Industries

Defense & Space

Resumes

Resumes

Frank Sciorelli Photo 1

Principle Product And Chief Engineer

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Location:
6175 Bridgeport Dr, Shingle Springs, CA 95682
Industry:
Defense & Space
Work:
Aerojet Rocketdyne
Principle Product and Chief Engineer
Education:
California Polytechnic State University - San Luis Obispo 1981 - 1985
Bachelors, Bachelor of Science, Mechanical Engineering

Publications

Us Patents

Heat Exchanger For A Rocket Engine

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US Patent:
20090218086, Sep 3, 2009
Filed:
Jun 26, 2008
Appl. No.:
12/147396
Inventors:
Frank A. Sciorelli - Cameron Park CA, US
Assignee:
AEROJET-GENERAL CORPORATION - Redmond WA
International Classification:
F28F 1/10
US Classification:
165181
Abstract:
A cylindrical rocket engine exhaust duct has a liner that fits inside an outer jacket. The outer periphery of the liner has circumferentially spaced ribs defining a sinuous path for a fluid to be heated. The liner has a least one, preferably several, transverse fins with internal serpentine passages for carrying the fluid to be heated through the fins. The fluid to be heated is directed around the periphery of the liner (between the liner and the jacket), and consecutively through the separate fins, along sinuous and serpentine paths for heating of the fluid by heat transfer from the exhaust gas of the rocket engine.
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Frank A Sciorelli from El Dorado Hills, CA, age ~62 Get Report