S
stevemilw
Guest
Hello, i was wandering if it would be possible to carry a rocket up to 100,000 feet using four weather balloons.
I am an engineer thinking of starting a business launching human cremations to the moon.
if i can harness the power of the balloon, the solid state fuel payload would be dreamtically reduced, allowing for the weight of the cremations to be placed in the rocket.
My question is, would the air be too thin at that altitude to provide enough resistance to create lift? In an ordinary rocket, does the speed of the rocket normally help it through the thin air, much like a slingshot? If this is the case then my idea may be flawed.
I have sketched down a release mechanism with a driver system to seperate the four balloons and open up a hole for the rocket dangling underneath to be launched. The teathers will be released apon the rocket rising above the balloons.
The preliminary stages would involve a prototype to get it into space, before worrying about guiding it to the moon.
What type of fuel do you think would be best for a system like this, im guesing none of you are really engineers here, but ill ask anyway. It woul need to be a high energy, fast output.
I am an engineer thinking of starting a business launching human cremations to the moon.
if i can harness the power of the balloon, the solid state fuel payload would be dreamtically reduced, allowing for the weight of the cremations to be placed in the rocket.
My question is, would the air be too thin at that altitude to provide enough resistance to create lift? In an ordinary rocket, does the speed of the rocket normally help it through the thin air, much like a slingshot? If this is the case then my idea may be flawed.
I have sketched down a release mechanism with a driver system to seperate the four balloons and open up a hole for the rocket dangling underneath to be launched. The teathers will be released apon the rocket rising above the balloons.
The preliminary stages would involve a prototype to get it into space, before worrying about guiding it to the moon.
What type of fuel do you think would be best for a system like this, im guesing none of you are really engineers here, but ill ask anyway. It woul need to be a high energy, fast output.