Building Real Scale Tiny Orbital Rockets 

Russian rocket engineers FIRED

Well, the shots would have been fired, but sadly the gun exploded... ;)

lol 😂

"Give me the N1 to free my soul, I wanna get lost in a fireball, and drift away.."

What book is it

I think I missed where he said the name

Name?

@@Ahblair4 Ignition

I'm personally a fan of the di-methyl mercury story, though the poor sulphur chemists being banished to a building literally miles away because of the smells was a highlight too.

Cody'sLab haha is there an unreal reality?

Love your stuff, keep it up Cody!

so there has to be a unity reality?

Amateur orbital rocketry! I love the idea.

Using gumweed fuel

I think he meant N1

Use ferram aerospace

Same true for US rocket development, dude. No difference at all.

Add more boosters

Jett Quasar soviet design tended to be so increadibly centralized that one single person was making the design decision, quality control, inspection procedures, launch conditions ect, it let them jump ahead with the r-7 and vostok but as rockets got more complicated this style became horrendously deficient as korolev's replacement was a raving alcoholic and had basically a competing space program within the soviet union. ironically this was the same thing that we did early on with vanguard and jupiter rocket programs but then we rightly recognized the need for one managable program and created NASA out of both and while it did have a director, design decisions were carried out by committee and time was taken for testing

+bergonius not sure why you're bringing up the US

In the beginning the US was like that but after the Apollo 1 disaster their quality control went way up. The N-1 suffered four failures in a row on a massive rocket, I don't think the American program would have survived such a disaster either.

Stellar Labs I know I’m a bit late but that’s easy, just leave the first stage on the pad attached to the launch clamps.

@@jamiesmith3396 That's not a suborbital path. Basically, the way to do this is make a giant SSTO that makes it almost to the mun, separate it after putting perigee below Earth's surface, then have a tiny spacecraft that burns a bit extra and goes and orbits the moon. This is just SSTO to the mun but easier.

SSTO lol

just make the first stage go into an escape trajectory

Gabe Snooks yeah me too what all happened to red dragon? :(

It's been canceled. Especially since they're no longer developing powered landings for Dragon V2. Like Scott mentioned Musk says there's a better way.

I think he decided instead of wasting money on 2 systems, just go for the gusto on the big boy. Even if it isnt hauling 100 people at a time, that is still alot of cargo capacity.

Yeah, that seems to be the consensus on r/spacex. The slightly smaller 9-meter version of ITS will likely be the first thing SpaceX sends to Mars, followed by the full-scale version.

Uhh... I built a 1.9 ton one...

Grant Exploit intrigued

from 13:00 onwards, it was "old" scott narrating. :D

old footage

Game got louder because I forgot to add a limiter to game audio.

Not when it's played at 10x regular speed.

this is not a scam

@@GalaxyGoldbox Who are you talking to?

@@StrangeScaryNewEngland That my friend is an excellent question!

@@StrangeScaryNewEngland The true meaning of that text has been long forgotten, as it was written in the days of yonder. It now serves merely as a reminder of better days.

@@GalaxyGoldbox Lmfao. You're alright in my book.

XxDeathSquadxX ouch

Yeah, sadly this becomes unwatchable. = (

nah raquel

PECHUNG!

That would be an interesting idea. What I know is that you need only 8500 m/s for very high TWR launchers and about 9500 m/s for very low TWR. My personal record is 8400 m/s to orbit.

How? What sort of launch profile are you using to get that low del v to orbit?

Very shallow ascent profile + high TWR rocket. Fly straight up to 50m/s, then start pitching down, it should look more or less like that: 50 m/s - pitch 89-90 350 m/s - pitch 62 1000 m/s - pitch 40 Next steps depends on TWR of your second stage. First stage TWR needs to be around 1.70 (surface). An example of such vehicle is my Saturn VB MLV used in my Ares Mission to Mars recreation.

That's a tricky optimisation problem. I think you need variational Lagrange multipliers and numerical integration.

winged love your videos mate.

Moshe Amezcua must have the RAM to hold it in.

You would just wait, as the orbits decay. Provided they are low enough anyway.

RancidMarshmallow until someone has a bfr launch that isn’t at the full capacity and you can piggyback on their launch.

It's Realism Overhaul. He just posted a video about installation with CKAN.

Check his video a few days ago about installing RSS+RO

Ignition

By John D. Clark, I believe?

Full Title: Ignition!: An informal history of liquid rocket propellants