ricardo__
Discord ID: 688104675571924998
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There was a car that somehow got there that got missed when they closed the roads
I love the red stone rocket engine
Yes it was watered down ethanol to not melt the engine
It uses water expansion for the turbo pump
*peroxide
Into steam to drive the pump
Those rockets practically ran on vodka they had to use a 70-30 mixture to keep things cool in the combustion chamber
How did the machine those metal parts before CNC
Yes
Mixing with water reduces efficiency , it’s only for the engine to not melt
How did they cool the lunar assent engine.
It had a pintle injecter
But how does a hypergolic not corrode the regen cooling channels
Yes
Is ammonia hypergolic with lox
Cough username cough
Lol
The proton is a weird rocket
And like 3 uperstages
All hypergolic
With a ISP of less than 290
And a horrible dry mass
Still
They wanted to launch human moon missions on that
When the n-1 hit the fan
And didn’t the have the NK-33 at that time
Haha ya
Even with kerosene you have a huge problem of a RUD
Methane or any other cryo boils away
If not combusted
Yes
Yes
And makes the engines have horrible engineering problems
With the TWR
Expander cycle is the best
Yes it’s too expensive if it’s not reused
And the rs68 failed to live up to its promises
A expander bleed cycle is the best option for a hydrolox first stage
It has good thrust and low complexity
It’s impossible to do that with a closed expander
For a first stage
True
It depends on your design consideration
The raptor is probably the the most complex modern engine
The pressures in the GG lines are 500+ bar oxygen
But the main advantage of a full flow is low turbo pump temps
Because one is so fuel rich and the other is so oxidizer rich
When it’s ready
That’s a scrub
Sn9 to fly tomorrow!!!
FAA with starship currently
T-38 inbound to boca chica!!!
The best airplane is the wb57 change my mind
SN9 is ready to fly
the FAA just scrubbed it
<:Thinking:798661678023573504>
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