About Skyroot Aerospace
A cuttingedge startup founded by exISRO scientists. Dedicated to affordable space access were rewriting aerospace technology rules. Our dynamic team fosters inventiveness collaboration and relentless excellence. Join us on a transformative journey to redefine space possibilities. Welcome to the forefront of space innovation with Skyroot Aerospace!
Essential Responsibilities:
Lead a dynamic team focused on designing efficient thermal systems for launch vehicles covering aerothermal analysis the design and validation of internal and external thermal protection systems (TPS) design and analysis of electronic packages etc.
Proven leadership in guiding crossfunctional teams through the design process ensuring successful thermal system integration and delivery for launch readiness.
Demonstrate strong systemlevel thinking and the ability to provide design recommendations based on simulation and experimental data to optimize thermal performance.
Preferred skills and experience:
Bachelors or Masters degree in Mechanical or Aerospace Engineering with a minimum of 10 years of relevant experience in the field.
Proven expertise in thermal modelling and analysis for both external/internal Thermal Protection Systems (TPS) and electronic package thermal design as well as solid/liquid rocket motor fluidthermal analysis.
Expertise in aerothermodynamics including proficiency in heat transfer thermodynamics and hightemperature material science specifically tailored to atmospheric reentry conditions supported by experience in computational tools and experimental techniques relevant to TPS design and validation.
Strong problemsolving skills with the ability to analyse challenges from a physical standpoint and deliver timely systemlevel solutions.
Demonstrated experience collaborating with crossfunctional teams to ensure designs meet all technical mission and safety requirements.
Good knowledge/experience in programming applied mathematics and highperformance computing CFD & FEA Modelling.
Skilled in developing and validating numerical models for reentry environments hightemperature combustion environments including ablative material behaviour and performance of active thermal protection systems using industrystandard programming languages such as MATLAB Python.
A commitment to staying uptodate with the latest advancements in aerospace thermal protection technologies and methodologies.