Senior Aerothermal Analysis Engineer

Benefits

Parental leave

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Non-birth-parent leave

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Family-building benefits

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Mental health support

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Relocation assistance

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Childcare support

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Market context

U.S. role benchmark (BLS OEWS)

$111,944 U.S. median for this role

Projected growth (BLS Employment Projections)

+13.7% - Much faster than average

Matched to SOC 15-1252 - Data and ML aggregate by role bucket.

Source: U.S. Bureau of Labor Statistics, OEWS, May 2024 and Employment Projections, 2024-2034.

Schedule

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Weekend work

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Application

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Deadline

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About this role

Senior Aerothermal Analysis Engineer Seattle, WA, United States, San Carlos, California Cowboy Space Corp. is building the infrastructure to power and connect the orbital economy. Our satellites operate in Low Earth Orbit to collect sunlight and enable a new class of capabilities-from powering on-orbit compute, to transmitting energy via infrared lasers (space-to-earth and space-to-space), powering on-orbit compute to delivering secure, high-bandwidth optical data. By rethinking how energy and data are generated and distributed in space, we're unlocking entirely new ways to operate both in orbit and on Earth. Founded in 2024 by Baiju Bhatt (co-founder of Robinhood), Cowboy Space Corp. is backed by leading investors and built by a team from top aerospace and defense organizations. We're moving quickly to solve complex technical challenges and build a new category of space infrastructure. The Role As an Aerothermal Analysis Engineer you will be the technical lead for predicting and managing the aerodynamic heating environments on the external surfaces of our new launch vehicle. This role will focus on predicting and characterizing the aerothermal environments experienced during ascent and re-entry, driving the boundary conditions that define the vehicle's external structures, including the main substrates and the required thermal protection system (TPS). This role can be located in Seattle WA or at our HQ in San Carlos. Responsibilities - Environment Definition: Generate high-fidelity aerodynamic pressure and heating environments, for nominal and off-nominal conditions, for launch vehicle's ascent and re-entry trajectories using engineering-level tools and Computational Fluid Dynamics (CFD) codes. - CFD Modeling &

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