Pablo Hollar
Co-Founder & CEO
Aerospace Engineer · UNLP, Argentina
M.Sc. Space Vehicle Design & Conception · ISAE–SUPAERO, France
MBA · UADE, Argentina
15 YRS IN THE SPACE INDUSTRY
STRUCTURAL & MECHANICAL DESIGN
SYSTEMS ENGINEERING FOR LAUNCH VEHICLES
Project Manager and Systems Engineer for launch vehicle programs at Argentina's national space agency. Expertise in structural and mechanical design across structures, avionics, and systems integration. M.Sc. from one of Europe's top aerospace institutions.
Pablo Reimonte
Co-Founder & CTO · Head of Propulsion
Aerospace Engineer · UNLP, Argentina
17 YRS IN LIQUID PROPULSION SYSTEMS
30+ LIQUID ROCKET ENGINES DESIGNED & TESTED
TEAM LEADERSHIP IN PROPULSION PROGRAMS
Designed and tested over 30 liquid rocket engines across multiple programs at CONAE and VENG S.A. (2008–2025). Thrust range from 83 kgf pressure-fed systems to 37,820 kgf turbopump-fed first-stage engines. Propellant experience spans N₂O₄/HNO₃, LOX/RP-1, and LOX/LCH₄. Led propulsion programs across design, manufacturing, and test operations. Built and operated four dedicated engine test facilities.