NYU Rogue Aerospace
NYU Rogue Aerospace
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Founder, Engineering Director, and Propulsion RE
Founder, Engineering Director, and Propulsion RE
Work Scope
Work Scope
Founder & Engineering Director:
Propulsion:
Ox Tank RE
GSE Fluids RE
Expected Test Operations Timeline:
Hydrostatic Test [February 2026]
Cold Flow Test [March 2026]
Static Fire(s) [April 2026]
Wet Dress Rehearsal [April 2026]
Program Progress
Program Progress
I am updating this section as things progress! All work shown here is my own but program wide work can be shown if requested.
Last Completed Program Milestone
Ox Tank Critical Design Review
Ox Tank Critical Design Review
Date Presented: November 2025
Summary: The presentation aims to get team–wide buy off on our first SRAD pressure vessel to hold 4.5 kg of N2O at a MEOP 1000psi.
Manufacturing: In progress currently
Drawings
Drawings
Updating drawings as project progresses and revisions are made.
[WIP] Fluids Modeling
[WIP] Fluids Modeling
Expected Release Date: February 2024
Summary: This presentation aims to cover an overview Fluids and CONOPS for our upcoming hydrostatic, cold flow, and static fire testing.
Current simulation results are plotted below
[WIP] GSE and Propulsion CONOPS + P&ID
[WIP] GSE and Propulsion CONOPS + P&ID
Expected Release Date: February 2024
Summary: This presentation aims to cover an overview of our GSE Fluids and CONOPS for our upcoming hydrostatic, cold flow, and static fire testing.
[WIP] Hydrostatic Testing
[WIP] Hydrostatic Testing
Expected Release Date: February 2024
Summary: This presentation aims to cover an overview of our GSE Fluids and CONOPS for our upcoming hydrostatic, cold flow, and static fire testing.
COTS Solids – NASA USLI Competition Documentation [Pre–Hybrid Rocket]
COTS Solids – NASA USLI Competition Documentation [Pre–Hybrid Rocket]
NASA CDR Competition 2024–25
NASA CDR Competition 2024–25
Engineering Directors: Teddy Polkosnik, Noel Kim, Karan S
NASA USLI: Developed a COTS Solid rocket on a L1520 to deliver an experimental payload to the dedicated altitude.
Result: Unable to go to competition.
Subscale Attempt 1: Recovery failure due to electronics failure
Subscale Attempt 2: Low thrust to weight ratio
Full-scale Attempt 1: Recovery failure due to improper electronics setting
Full-scale Attempt 2: CATO
Fixed: Before taking on the hybrid rocket program we have eliminated all of these issues on our subscale demonstrator - Pathfinder [November 2024]
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