Awards & Nominations
Helios Space has received the following awards and nominations. Way to go!

Helios Space has received the following awards and nominations. Way to go!
We propose a novel approach to fabricate carbon nanotubes (CNT) utilizing in-situ atmospheric CO2 from the Venusian atmosphere to create a tethered balloon, which would enable a temperature differential, leveraged by a thermoelectric generator to produce constant power for the lander system. It is important to both NASA and Earth to work on the mass manufacturing capabilities of carbon nanotubes to enable strong lightweight and highly conductive materials that provide multiple benefits here on Earth and in our mission to travel the stars, ranging from space elevators to high capacity energy storage systems.
We propose a novel approach to fabricate carbon nanotubes (CNT), via a wet-spin process, utilizing in-situ atmospheric CO2 from the Venusian atmosphere to create a tethered balloon, which would enable a temperature differential, leveraged by a thermoelectric generator to produce constant power for the lander system. Then we propose an extension whereby, with a sufficiently strong tether, a balloon is sent to capture sulfuric acid and extract its H2 to be used in hydrogen fuel cells or with hydroxide exchange membrane fuel cells (HEMFC) to extract atmospheric CO2 and generate power.
We used TinkerCAD to develop the CAD model.
We used the information provided in the NIAC Phase 1 Final Report: Venus Landsailer Zephyr extensively to understand the challenges in a spacecraft designed for the Venusian surface.
The initial idea of the CO2 ISRU approach was to use hydroxide exchange membrane fuel cells (HEMFC) to extract the CO2 for the lower atmosphere to generate energy. After an analysis of the chemical reaction equations, we determined that key components necessary for the reaction to occur are not available on the surface of Venus, but in its atmosphere. Specifically, the sulfuric acid clouds, which lead us down the path of a tethered balloon system via carbon nanotube manufacturing. But after further investigation, we determined that the wind speeds at that altitude would be catastrophic for the balloon and the tether system. We finally realized that if we go lower in the atmosphere, we could leverage the temperature difference with a thermoelectric generator.
#CO2, #ISRU, #Venus, #hardware, #Power, #TEG, #CNT
Your challenge is to design an energy storage system that will power a surface lander or rover on the surface of Venus for at least 60 days, so that there is a viable energy storage capability for long-duration exploration missions.
