Dave Gingerich

Dave Gingerich

Denver Metropolitan Area
15K followers 500+ connections

About

In 40 years at Lockheed Martin, Sr Staff Engineer Dave Gingerich has had several “jobs of…

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Contributions

Activity

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Experience

Education

  • Webster University Graphic
  • -

    Activities and Societies: part-time work for a solar energy forecasting company

    applied optimal control through EE department, along with solar energy and solar village courses through ME dept.

  • -

    Activities and Societies: KWCW FM Radio, CELL (student-faculty evening social group)

    Nearly a double major in math and physics. Short one 3 hour course in physics.

Volunteer Experience

  • Community Resources, Inc. Graphic

    Classroom speaker

    Community Resources, Inc.

    - Present 16 years 1 month

    Science and Technology

    Entertaining, educational and inspirational presentations on space exploration, the solar system and space careers to students in Denver Public Schools from Early Childhood Education thru high school.
    Also, having some of the most fun I've ever had!

Publications

  • The Russian R-16 Nedelin Disaster: An Historical Analysis of Failed Safety Management

    Journal of Space Safety Engineering – Vol. 2 No. 2 - December 2015

    On October 24, 1960, at the USSR's Baikonur Cosmodrome, an electrical malfunction led to the deadliest launch accident in space industry history. Shortly before a test launch of the first Soviet R-16 intercontinental rocket, the second stage engines prematurely ignited, detonating the first stage fuel tanks. We hypothesize that the primary contributing factor to the tragedy was a systemic flaw in safety management caused by cultural and political values. Through the use of interviews…

    On October 24, 1960, at the USSR's Baikonur Cosmodrome, an electrical malfunction led to the deadliest launch accident in space industry history. Shortly before a test launch of the first Soviet R-16 intercontinental rocket, the second stage engines prematurely ignited, detonating the first stage fuel tanks. We hypothesize that the primary contributing factor to the tragedy was a systemic flaw in safety management caused by cultural and political values. Through the use of interviews, literature, and a chronology of the events leading up to the failure, an interpretive analysis identifying contributing factors to the disaster was conducted. This study found that cultural and political influences were primary causes to the loss and also let to a safety management environment that continued to threaten the success and integrity of aerospace development in the USSR and other space-faring countries.

    Other authors
    See publication
  • Verification of Mars Odyssey All-Stellar Attitude Determination Ten Years After Launch

    2015 IEEE Aerospace Conference, Big Sky, MT

  • Resource Planning for Long-Duration Space Missions

    IEEE Space Mission Challenges for Information Technology International Conference, Johns Hopkins, Laurel, Maryland

  • Expanding Our Perspective of the Nedelin Disaster of 1960

    AIAA Space Conference, August 2014, San Diego, California

  • Verification of Mars Odyssey Flight Software Ten Years After Launch

    AIAA SpaceOps International Conference, Pasadena, California

  • Mission Risk Evaluation and Communications Tool

    AIAA Space Conference, September 2008, San Diego, California

  • Resource Planning Considerations for Long-Duration Space Missions

    AIAA Space Conference, September 2008, San Diego, California

  • Asteroid 5535 Annefrank size, shape, and orientation: Stardust first results

    JOURNAL OF GEOPHYSICAL RESEARCH, VOL. 109, E02002, doi:10.1029/2003JE002108, 2004

    The NASA Discovery Stardust spacecraft flew by the main belt asteroid 5535 Annefrank at a distance of 3100 km and a speed of 7.4 km/s in November 2002 to test theencounter sequence developed for its primary science target, the comet 81P/Wild 2.During this testing, over 70 images of Annefrank were obtained, taken over a phase anglerange from 40 to 140 deg. This viewing showed that Annefrank was at least 6.6

    5.0

    3.4 km in size (diameters), with its shortest dimension normal to its…

    The NASA Discovery Stardust spacecraft flew by the main belt asteroid 5535 Annefrank at a distance of 3100 km and a speed of 7.4 km/s in November 2002 to test theencounter sequence developed for its primary science target, the comet 81P/Wild 2.During this testing, over 70 images of Annefrank were obtained, taken over a phase anglerange from 40 to 140 deg. This viewing showed that Annefrank was at least 6.6

    5.0

    3.4 km in size (diameters), with its shortest dimension normal to its orbit plane. Annefrank is highly angular, with flat appearing surfaces, possibly planes formed when it wasfractured off of a larger parent body. For the limited part of the surface seen, Annefrank resembles a triangular prism for the main body, with smaller, rounder bodies, possiblyaccreted through contact.

    Other authors
    • Thomas C. Duxbury
    • Ray L. Newburn
    • Donald E. Brownlee
    • Susan J. Mumaw
    • Stephen P. Synnott
    • Charles H. Acton
    • Eric Carranza
    • Timothy P. McElrath
  • Genesis On-Board Determination of the Solar Wind Flow Regime

    Space Science Reviews, January 2003, Volume 105, Issue 3, pp 661–679

    Some of the objectives of the Genesis mission require the separate collection of solar wind originating in different types of solar sources. Measurements of the solar wind protons, alpha particles, and electrons are used on-board the spacecraft to determine whether the solar-wind source is most likely a coronal hole, interstream flow, or a coronal mass ejection. A simple fuzzy logic scheme operating on measurements of the proton temperature, the alpha-particle abundance, and the presence of…

    Some of the objectives of the Genesis mission require the separate collection of solar wind originating in different types of solar sources. Measurements of the solar wind protons, alpha particles, and electrons are used on-board the spacecraft to determine whether the solar-wind source is most likely a coronal hole, interstream flow, or a coronal mass ejection. A simple fuzzy logic scheme operating on measurements of the proton temperature, the alpha-particle abundance, and the presence of bidirectional streaming of suprathermal electrons was developed for this purpose. Additional requirements on the algorithm include the ability to identify the passage of forward shocks, reasonable levels of hysteresis and persistence, and the ability to modify the algorithm by changes in stored constants rather than changes in the software. After a few minor adjustments, the algorithm performed well during the initial portion of the mission.

    Other authors
    • Neugebauer M
    • Steinberg J.T.
    • Tokar R.L.
    • Barraclough B.L.
    • Wiens R.C.
    • Whiteaker D.B.
    • Dors E.E.
    • Luckey D.
  • Phase curve and albedo of asteroid 5535 Annefrank

    JOURNAL OF GEOPHYSICAL RESEARCH, VOL. 108, NO. E11, 5117, doi:10.1029/2003JE002106, 2003

    Seventy-two images of the S-class asteroid 5535 Annefrank, acquired on 2 November 2002 at target ranges of 11,415–3078.5 km, were transmitted to Earth as a part of an engineering readiness test of the Stardust mission. Forty-four of these were used to create a phase curve extending to 134°, the largest angle yet achieved for any S-class asteroid. Flux fell by more than six magnitudes between the extrapolated 0° and 134°. A maximum illuminated cross section of 16 km2 was seen at a phase angle of…

    Seventy-two images of the S-class asteroid 5535 Annefrank, acquired on 2 November 2002 at target ranges of 11,415–3078.5 km, were transmitted to Earth as a part of an engineering readiness test of the Stardust mission. Forty-four of these were used to create a phase curve extending to 134°, the largest angle yet achieved for any S-class asteroid. Flux fell by more than six magnitudes between the extrapolated 0° and 134°. A maximum illuminated cross section of 16 km2 was seen at a phase angle of 47.2°. Assuming a camera efficiency of 75%, a broadband (470–940 nm) geometric albedo of 0.24 was derived for Annefrank

    Other authors
    • Ray L. Newburn Jr.
    • Thomas C. Duxbury
    • Donald E. Brownlee
    • Martha Hanner
    • Shyamkumar Bhaskaran
    • Edward E. Hirst
    • Ramachand S. Bhat
    • Tseng-Chan M. Wang
    • Peter Tsou
    • Susan J. Mumaw
  • Spacecraft Automated Electrical Power Subsystem Simulator

    18th Intersociety Energy Conversion Engineering Conference

  • IEEE Transactions on Aerospace and Electronic Systems

    IEEE

    Peer reviewer for published papers

Courses

  • Aerospace Commercialization

    AES 4602

  • Aerospace Operations Systems Analysis and Design

    AES 4603

  • Capstone

    SPSM 6000

  • Dynamics and Orbital Mechanics

    SPSM 5740

  • Space Environment

    SPSM 5000

  • Space Flight Ops I

    AES 3600

  • Space Flight Ops II

    AES 4601

  • Space Mission Operations

    SPSM 5770

  • Space Systems Engineering

    SPSM 5750

  • Space Systems Integration

    SPSM 5910

  • Space Systems Operations Research

    SPSM 5730

  • Special Topics: Spaceflight Hazards

    SPSM 5990

Projects

  • Mars One 2018 Lander University Payload Competition

    • Assisted with management of payload project, including task assignment, scheduling and document analysis
    • Helped design physical structure of payload to meet Mars One competition requirements
    • Grew project team and advisors by utilizing network of resources
    • Assisted with payload proposal writing and editing
    • Developed working principle of payload and its systems
    • Helped with communications and marketing of payload during second round of competition
    • Will continue to…

    • Assisted with management of payload project, including task assignment, scheduling and document analysis
    • Helped design physical structure of payload to meet Mars One competition requirements
    • Grew project team and advisors by utilizing network of resources
    • Assisted with payload proposal writing and editing
    • Developed working principle of payload and its systems
    • Helped with communications and marketing of payload during second round of competition
    • Will continue to help in management of payload development and functional testing in an advisory manner as a club alumnus

    Other creators
    See project
  • Interdisciplinary Mock Mars Mission

    - Present

    A successful manned mission to Mars - followed by colonization - is going to entail much more than just putting a few astronauts on a ship and sending them on their way. It will require people from every discipline to communicate, plan and organize with a common goal in mind.

    My mock Mars mission project is based on my belief that it will take more than the, "hard," sciences to get man to Mars and that great care should be taken to establish a base or colony that will include a cross…

    A successful manned mission to Mars - followed by colonization - is going to entail much more than just putting a few astronauts on a ship and sending them on their way. It will require people from every discipline to communicate, plan and organize with a common goal in mind.

    My mock Mars mission project is based on my belief that it will take more than the, "hard," sciences to get man to Mars and that great care should be taken to establish a base or colony that will include a cross section of the human culture. Mars is for Earthlings, not nations.

    This project is open to every student at the Metropolitan State University of Denver, regardless of major, because every field of study will be able to provide answers to the plethora of questions that arise from asking the much simpler question, "can we do it?"

    With the help of a faculty advisor and myself, participants will conduct their own research as it pertains to the mission. They will be required to communicate their findings to other participants and collaborate with students outside of their field as they conduct their research.

    This project is currently in the recruitment phase with our preliminary meeting happening Monday, November 18th. The project will span the Spring 2014 and Fall 2014 semesters giving students ample time to conduct their research without compromising their regular coursework.

    Other creators
  • The Russian R-16 Nedelin Disaster: An Historical Analysis of Failed Safety Mangement

    -

    Paper regarding the events leading to the R-16 Nedelin disaster in 1960.

    Other creators

Honors & Awards

  • Panelist for STEM Day at Colorado State Capital

    Colorado Succeeds and South Denver Metro Chamber

    One of four panelists discussing STEM (Science, Technology, Engineering, and Math) Education in Colorado in the Old Colorado Supreme Court Chambers in the Colorado State Capital Building.
    Panel was sponsored by Colorado Succeeds and the South Denver Metro Chamber

Organizations

  • SSPI (Society of Satellite Professionals International)

    -

    - Present
  • IAASS, (International Association for the Advancement of Space Safety)

    -

    - Present
  • Planetary Society

    -

    - Present
  • AIAA (American Institute of Aeronautics and Astronautics)

    Member

    - Present
  • ACM (Association for Computing Machinery)

    -

    -

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