David Januzzi

David Januzzi

Merritt Island, Florida, United States
604 followers 500+ connections

About

Launch Vehicle Operations Engineer (Cryogenics/Pneumatics) at Blue Origin, working toward…

Activity

Join now to see all activity

Experience

  • Blue Origin Graphic

    Blue Origin

    Cape Canaveral, FL

  • -

    Cape Canaveral, Florida, United States

  • -

    Cape Canaveral, Florida, United States

  • -

    Kennedy Space Center, Florida

  • -

    Kennedy Space Center, Florida

Education

  • The Ohio State University Graphic

    The Ohio State University

    3.23

    -

    Activities and Societies: - Member of the AIAA student chapter - Co-team lead for the Recovery Systems sub-team for The Buckeye Space Launch Initiative at The Ohio State University

Licenses & Certifications

Courses

  • Advanced Space Propulsion

    AAE 5752

  • Applied Computational Fluid Dynamics and Heat Transfer

    ME 5539

  • Design of Atmospheric Flight Vehicles

    AAE 4515 and 4516

  • Experimental Projects

    AAE 4510 and 4511

  • Flight Vehicle Controls

    AAE 3521

  • Flight Vehicle Dynamics

    AAE 3520

  • Flight Vehicle Structures I

    AAE 3542

  • Flight Vehicle Structures II

    AAE 3543

  • Fundamentals of Aerodynamics

    AAE 3560

  • Guidance, Navigation and Conrtol of Aerospace Vehicles

    AAE 5621

  • Heat Transfer

    AAE 3580

  • Numerical Methods

    AAE 3581

  • One-Dimensional Gas Dynamics

    AAE 3570

  • Principles of Propulsion

    AAE 4550

Projects

  • Carrier-Based Supersonic Unmanned Escort Strike Fighter

    - Present

    This project is for the Design of Atmospheric Flight Vehicles course that I am currently taking. This is a two semester long design project were myself and 5 other classmates make up a team who's goal is to develop a design for a Carrier-Based Supersonic Unmanned Escort Strike Fighter. The design is to be based on the desired qualities and parameters as defined by our instructor (Which includes having a dash speed of at least Mach 2.0, having super cruise capability, and being able to…

    This project is for the Design of Atmospheric Flight Vehicles course that I am currently taking. This is a two semester long design project were myself and 5 other classmates make up a team who's goal is to develop a design for a Carrier-Based Supersonic Unmanned Escort Strike Fighter. The design is to be based on the desired qualities and parameters as defined by our instructor (Which includes having a dash speed of at least Mach 2.0, having super cruise capability, and being able to withstand +12 and -8 g's of force). I am the Propulsion technical lead, where i am responsible for the design of the propulsion systems for the aircraft, which includes determining the engine to use, analyzing the engine, design the engine inlets, incorporating thrust vectoring (if the teams deems to be necessary), and the fuel systems integration. In addition all of the members are responsible for conduction structural analysis of the aircraft design.

  • Stand Up Paddleboard High Performance Design

    - Present

    This team project is part of the Aerospace Engineering capstone course (Experimental Projects, AAE 4510-4511) and is a two semester long project. Myself and the rest of team are setting out to engineer and design a race quality paddleboard that has less drag than existing board (Making it a faster board). We will develop a testing procedure in order to determine the drag on current racing boards. The testing will use both computational tests (mainly CFD), and experimental testing (testing the…

    This team project is part of the Aerospace Engineering capstone course (Experimental Projects, AAE 4510-4511) and is a two semester long project. Myself and the rest of team are setting out to engineer and design a race quality paddleboard that has less drag than existing board (Making it a faster board). We will develop a testing procedure in order to determine the drag on current racing boards. The testing will use both computational tests (mainly CFD), and experimental testing (testing the boards in the water to find the drag coefficient). From those results the team will set out to develop a new board that has a lower drag coefficient than existing boards.

  • The Buckeye Space Launch Initiative

    I am a Co-Team Lead for the Recovery Systems sub-team for this student run competition team. There are three current projects which include the 30k competition rocket, the 10k competition rocket, and the Space Launch Initiative Project. Myself and the other lead are in charge of the recovery systems design and manufacturing for all three of the current projects. We lead a small group of fellow students, and the projects within the team include, parachute design, parachute manufacturing, flow…

    I am a Co-Team Lead for the Recovery Systems sub-team for this student run competition team. There are three current projects which include the 30k competition rocket, the 10k competition rocket, and the Space Launch Initiative Project. Myself and the other lead are in charge of the recovery systems design and manufacturing for all three of the current projects. We lead a small group of fellow students, and the projects within the team include, parachute design, parachute manufacturing, flow simulation (using CFD), and general recovery systems research for future designs to name a few.

    See project

Honors & Awards

  • Artemis I Launch Director Award

    Artemis I Launch Director - Charlie Blackwell-Thompson

    Received Launch Director Award for Artemis 1 for leading the ICPS Helium Check Valve Failure Non-Conformance resolution effort (initial troubleshooting at the PAD, developing con-ops and rationale to proceed into Wet Dress Rehearsal #3, developing contingency plans for vehicle rollback to VAB, leading the intrusive inspections and troubleshooting of the helium system in the VAB, implementing corrective actions, leading the retest effort in the VAB, and certifying the system for additional…

    Received Launch Director Award for Artemis 1 for leading the ICPS Helium Check Valve Failure Non-Conformance resolution effort (initial troubleshooting at the PAD, developing con-ops and rationale to proceed into Wet Dress Rehearsal #3, developing contingency plans for vehicle rollback to VAB, leading the intrusive inspections and troubleshooting of the helium system in the VAB, implementing corrective actions, leading the retest effort in the VAB, and certifying the system for additional tanking tests and eventually for flight).

  • Spaceflight Processing Director's Award

    Director of TOSC Spaceflight Processing

  • Fall 2016 Dean's List

    The Ohio State University College of Engineering

    Made the Dean's List for the Fall 2016 semester for having a semester GPA greater than 3.5 (Had 3.587)

Languages

  • English

    -

More activity by David

View David’s full profile

  • See who you know in common
  • Get introduced
  • Contact David directly
Join to view full profile

Other similar profiles

Explore top content on LinkedIn

Find curated posts and insights for relevant topics all in one place.

View top content

Add new skills with these courses