per 1000 liters its about 550 liters fuel and its about 18.57 kg of structure per area of fuel tank. Now its time to figure out of threshold of diameters to include in rocket design parameters.
After some tinkering I found out, fuel tank mass is related to its area and not its volume. pretty much on low volume tanks doesn't benefit from low density fuel.
per 1000 liters its about 550 liters fuel and its about 18.57 kg of structure per area of fuel tank. Now its time to figure out of threshold of diameters to include in rocket design parameters.
1.8 years agoAfter some tinkering I found out, fuel tank mass is related to its area and not its volume. pretty much on low volume tanks doesn't benefit from low density fuel.
1.8 years ago