|
·
Fluid system design and analysis – gas,
liquid, two-phase
·
Heat transfer and thermodynamic analysis of
process systems for application
·
Thermal analysis input for structural analysis
and design
·
Spacecraft, launch vehicle – internal flow
field cooling
·
Propulsion system analysis and rocket
performance using ROCETS code
·
Tools:
PRO-E, SINDA-G, SIM-FLEX II DeltaE, Pro-E, Nevada, Regen, and in-house
software
·
Flight test and analysis of propulsion and fuel systems for aircraft
(Boeing 757, 767, 747, B2-Bomber)
·
Flight test and analysis of propulsion, fuel
systems, and abort systems for spacecraft (orbital space plan, evolved
expendable launch vehicle)
|

Multi-cryo storage
tank design for spacecraft
|