That guy had one of the top 5 comedy shows on TV ever.This is actually a pretty goddamn good critique on life these days… it actually is related lol…
That was a Delta, note solid boosters and large payload fairingWanna watch one more time @cannabineer
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Well, there’s a Delta for ya.That was a Delta, note solid boosters and large payload fairing
The Delta IV Heavy is the only version still flying, usually with a defense payload. The cost per launch is listed as $164+ million. The Falcon 9 is $62 million per launch with comparable payload to orbit. SpaceX is setting up to be very competitive.Well, there’s a Delta for ya.
See this is why I hangout here. I learn so much. LolThe Delta IV Heavy is the only version still flying, usually with a defense payload. The cost per launch is listed as $164+ million. The Falcon 9 is $62 million per launch with comparable payload to orbit. SpaceX is setting up to be very competitive.
I dunno. If they get Starship and its booster stage running well soon, it could be a game changer. So far their engineering has been quite good.Space X honestly needs to concentrate on ISS and the moon first then mars. Or at least ISS to use it as a launch platform.
Honestly your right bout the engineering so far. Imagine if they got they're hands on ion engines..and added them.I dunno. If they get Starship and its booster stage running well soon, it could be a game changer. So far their engineering has been quite good.
Unfortunately ion engines (Star Trek notwithstanding) have some real disadvantages. They use lots of electrical energy to produce very low thrust. The propellant of choice, xenon, is very expensive.Honestly your right bout the engineering so far. Imagine if they got they're hands on ion engines..and added them.
I always thought xenon was fairly inexpensive. Now the energy to fuel, miniature nuke reactors. There already a satellite that has an example for the tech out in space now. The tech is out there, just how to use it.Unfortunately ion engines (Star Trek notwithstanding) have some real disadvantages. They use lots of electrical energy to produce very low thrust. The propellant of choice, xenon, is very expensive.
The NSTAR thruster on the Deep Space 1 mission used 2 kW to generate a third of an ounce of thrust. Its specific impulse was about 3000 seconds.
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