What does to the moon mean here? In orbit? It will take more dV to get a payload onto the moon from the earth than it will to Mars since Mars has an atmosphere that you can dump all of that transfer dV into while in the case of the moon you need to have that dV onboard.1 costs MORE delta V to get to the lunar surface than it does to land on Mars.
2 see above as for financially add the fact that Ice processing infrastructure on Luna isnt free and hydrolox has horrible mass ratio,
Wait, what? I'm pretty sure I've seen stated "payload to moon" with bigger figures than to Mars. On a quick check, yes indeed you need some 3.2km/s for TLI and 3.8km/s for TMI, not to mention you've got twice as much gravity to handle in Mars as opposed to Moon.
Congratulations to Congresswoman Kenda Horn (D) of Oklahoma. I hope your constituents become well aware of your efforts to stifle competition, waste our tax dollars, and coddle to a massive defense contractor.
Even if you want to get in orbit, it’s possible (although not yet attempted) to aerocapture with a very modest burn to circularize.What does to the moon mean here? In orbit? It will take more dV to get a payload onto the moon from the earth than it will to Mars since Mars has an atmosphere that you can dump all of that transfer dV into while in the case of the moon you need to have that dV onboard.1 costs MORE delta V to get to the lunar surface than it does to land on Mars.
2 see above as for financially add the fact that Ice processing infrastructure on Luna isnt free and hydrolox has horrible mass ratio,
Wait, what? I'm pretty sure I've seen stated "payload to moon" with bigger figures than to Mars. On a quick check, yes indeed you need some 3.2km/s for TLI and 3.8km/s for TMI, not to mention you've got twice as much gravity to handle in Mars as opposed to Moon.
The following solar system subway map (not the most correct) but still helpful. Note the arrows denoting aerobraking, that means most of the dV needed for that segment could be avoided using the atmosphere.
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You seem to be agreeing with me in a way that makes it sound like you are disagreeing.You need massive funding to get a crew to and from Mars.
Not that massive for a cost-optimized effort. Tens of billions, probably, but much less then hundreds. Many companies and some individuals could do it right now, and even more when someone perfects fully reusable rockets.
Case and point: SpaceX already building a prototype while the government is celebrating a accomplishment that was never impressive to anyone but the people with blinders on (late and over budget). The government is behind the curve already, so "money" doesn't seem to be the sole factor (or the key one).
Money in =/= quality or efficiency, not when the government is directly involved. You get some competition though, and when this boondoggle fails, heads roll since there is a measuring stick. At the very least, it motivates lean spending and accountability. The reason these House members keep getting reelected is because they can hide behind "no alternatives", but SpaceX has exposed a ton of their corruption by doing what they've failed (intentionally) to do for decades, quicker, safer, cheaper. Proving that you DON'T need government to do this stuff (once upon a time, sure, but the government has recently been systematically chasing off all the experts that knew how and replacing them with yes-men empty suits...).
I agree there's signifigant bloat.
I laud the efficiency and innovation of SpaceX in particular.
I consider "tens of billions of dollars" to be "significant funding"
Significant, but not outside the range of other private aerospace projects. Airbus spent $25B developing A380. Boeing typically spends $15B developing a new airliner.
Airbus has sold 6 A380s since 2015 and has had 72 order cancellations in that time. Production will end at 251 with the last delivery in 2021. They basically broke even on production, but the $25 billion development cost was a near total loss. Had Emirates not bought 123 of them, it would have been a complete flop.With the expectation, that they sell lot of A380s and recoup that money with profit on top. What is the recoup and profit on SpaceX spending say 50 billion OF THEIR OWN MONEY in developing and launching mission to Mars.
And if we need to "prove technologies" do them in LEO or on rovers or automated facilities at either destination. There's not much to be gained bootstrapping one destination to the other.You can't keep changing plans and expect something to be accomplished. The moon is a jumping point to Mars, at some point we can have a small moon base to refuel rockets on their way to Mars. Let NASA work on the moon while SpaceX and Boeing work towards Mars.
The purpose to go to the moon is to go to the moon. If you want to go to Mars just go to Mars. Going to the moon to go to Mars makes no damn sense. That being said pick one and go there. This continual changing of destinations ensures we will go to neither which I guess is part of the point.
I will say that going to Mars first pretty much means going anywhere in the Solar System after that. Because it means you've mastered on-orbit refueling and multi-month transits.
Airbus has sold 6 A380s since 2015 and has had 72 order cancellations in that time. Production will end at 251 with the last delivery in 2021. They basically broke even on production, but the $25 billion development cost was a near total loss. Had Emirates not bought 123 of them, it would have been a complete flop.With the expectation, that they sell lot of A380s and recoup that money with profit on top. What is the recoup and profit on SpaceX spending say 50 billion OF THEIR OWN MONEY in developing and launching mission to Mars.
That would be perfectly in line with Congress' lunar base plans!Aside from the previously-mentioned water ice, there's also helium-3, which might be useful in more advanced fusion reactors. (This presumes that we can get currently-planned reactors to work right.)What is there on the moon that is so valuable for there to be a land rush? I've always been under the impression that the moon's most useful feature is its gravity.
I'm confident that we'll get the currently planned fusion reactors working in twenty years.
Ask me next year and the answer will be the same.
Even if you want to get in orbit, it’s possible (although not yet attempted) to aerocapture with a very modest burn to circularize.
Why would you take lunar ice to LEO, it is far less costly in money and delta v to launch the prop from Earth where it is far cheaper and you have more useful options.
Less money for sure not less DeltaV (2.74 km/s vs 9.30 km/s). To be clear I am not advocating lunar ice mining that is cart way before the horse.
Looking at that map, why's the dV to get to the surface of Venus from low orbit so large (27 km/s) ? Now, yes, aerobreaking would be of considerable benefit for Venus, but still, that diagram suggests that the total dV budget to land on Venus would be substantially more than to land on Mercury, which seems counter-intuitive.The following solar system subway map (not the most correct) but still helpful. Note the arrows denoting aerobraking, that means most of the dV needed for that segment could be avoided using the atmosphere.
I think you meant shed the speed aerodynamically.1 costs MORE delta V to get to the lunar surface than it does to land on Mars.
2 see above as for financially add the fact that Ice processing infrastructure on Luna isnt free and hydrolox has horrible mass ratio,
Wait, what? I'm pretty sure I've seen stated "payload to moon" with bigger figures than to Mars. On a quick check, yes indeed you need some 3.2km/s for TLI and 3.8km/s for TMI, not to mention you've got twice as much gravity to handle in Mars as opposed to Moon.
It takes more energy to get to Mars orbit than lunar orbit but he wasn't talking about going to orbit he was talking about going to the surface. The moon has no atmosphere so all the DeltaV has to come propulsively. Mars landing can use the atmosphere for a significant portion reducing the DeltaV required propulsively.
It is about 6 km/s DeltaV from LEO to lunar surface and there is no way to reduce that. In fact the safer indirect route through LLO raises it a few hundred meters per second. It is about 10.0 km/s from LEO to Mars surface but you can shed about 6 km/s of that propulsively meaning your propulsive requirements are about 4 to 5 km/s. SpaceX BFR can do it with as little as 5 km/s in the tank at LEO and that includes a bit of a reserve.
Venus has an incredibly thick, dense atmosphere. That could be drag/gravity losses. You'll note that Earth is listed as 9.4km/s required, even though LEO energy is only ~8km/s. It could be an "adjusted" value accounting for the fact that ambient pressure makes rocket motors nearly useless on the Venusian surface. It could be that it's a map for a video game mod (KSP + RSS), and the extreme conditions of the planet are not well modeled by the game engine.Looking at that map, why's the dV to get to the surface of Venus from low orbit so large (27 km/s) ? Now, yes, aerobreaking would be of considerable benefit for Venus, but still, that diagram suggests that the total dV budget to land on Venus would be substantially more than to land on Mercury, which seems counter-intuitive.The following solar system subway map (not the most correct) but still helpful. Note the arrows denoting aerobraking, that means most of the dV needed for that segment could be avoided using the atmosphere.
(Or does this fit your "not the most correct" comment about the diagram ?)
More like you need to outbid Boing....not an easy task.Is this bill at the stage where we should start contacting our reps?
Unless you attach a hefty check along with your email, your rep is going to be completely deaf to anything you say. As they say, money talks, bullshit walks.
the most important number is cost, you need infrastructure that doesnt even exist yet on lunaWhy would you take lunar ice to LEO, it is far less costly in money and delta v to launch the prop from Earth where it is far cheaper and you have more useful options.
Less money for sure not less DeltaV (2.74 km/s vs 9.30 km/s). To be clear I am not advocating lunar ice mining that is cart way before the horse.
Delta-V is only one part of the calculation when comparing Earth vs Moon surface to LEO. Earth has 6x the gravity and it has an atmosphere.
A huge chunk of the fuel launching from Earth is spent lifting the engines and the fairing. Lower gravity means lower thrust, which means smaller, lighter & cheaper engines. The actual Moon->Earth transfer can even be done with ultra-efficient electric engines which are useless for leaving Earth.
There are massive obstacles and infrastructure requirements, of course, and if Starship pans out that will drastically reduce the cost of Earth-to-LEO. But looking several decades ahead, the country that is ahead in Lunar (or potentially asteroid, I'll grant you) fuel production will be the one that is sending millions to Mars and beyond by the end of the century.
And the exploration towards that Lunar/asteroid build-up is starting now, just not by NASA.
Why would you take lunar ice to LEO, it is far less costly in money and delta v to launch the prop from Earth where it is far cheaper and you have more useful options.
This is your space program run by bureaucrats and politicians with advice from lobbyists. Any questions?
Why would you take lunar ice to LEO, it is far less costly in money and delta v to launch the prop from Earth where it is far cheaper and you have more useful options.
Getting it to LEO from Earth isn't less costly, if you need five launches to refuel Starship, you're spending vast majority of your fuel for lift, not payload.
You do realize you don't have to process the water in the moon? Just ship it as it is, you can do the electrolysis in LEO as needed, as a bonus you don't have a 2 week night to deal with. Space(X) orbital gas station now open for business with low low cost on water, oxygen and hydrogen..
Are you maybe somehow building those rockets out of Lunar regolith?Why would you take lunar ice to LEO, it is far less costly in money and delta v to launch the prop from Earth where it is far cheaper and you have more useful options.
Getting it to LEO from Earth isn't less costly, if you need five launches to refuel Starship, you're spending vast majority of your fuel for lift, not payload.
You do realize you don't have to process the water in the moon? Just ship it as it is, you can do the electrolysis in LEO as needed, as a bonus you don't have a 2 week night to deal with. Space(X) orbital gas station now open for business with low low cost on water, oxygen and hydrogen..
https://science.house.gov/imo/media/doc ... 01_xml.pdf
Ms. KENDRA S. HORN of Oklahoma (for herself, Mr. BABIN, Ms. JOHNSON of Texas, and Mr. LUCAS) introduced the following bill
Two Dems and two Rs. Bipartisan sponsorship.
or launching a bunch of SS without payload to transfer prop into the departing SSAre you maybe somehow building those rockets out of Lunar regolith?Why would you take lunar ice to LEO, it is far less costly in money and delta v to launch the prop from Earth where it is far cheaper and you have more useful options.
Getting it to LEO from Earth isn't less costly, if you need five launches to refuel Starship, you're spending vast majority of your fuel for lift, not payload.
You do realize you don't have to process the water in the moon? Just ship it as it is, you can do the electrolysis in LEO as needed, as a bonus you don't have a 2 week night to deal with. Space(X) orbital gas station now open for business with low low cost on water, oxygen and hydrogen..
You see, to lift the water from the Moon you first need to get the rockets there somehow, meaning you launch them from Earth anyway, packed with fuel instead of water. Might need to refuel on LEO anyway. Then you use some of that fuel to land on the Moon and the rest of it launching again with the water, flying back to LEO and parking there. How is that supposed to be less costly than just lifting the water from Earth to LEO in the first place?
the most important number is cost, you need infrastructure that doesnt even exist yet on luna
There was a joke on one of these discussions recently that space is uphill bothways. That might be true for gravitational effects, but it isn't true for atmospheric effects - a thick atmosphere is detrimental on departure, but advantageous on arrival. That would seem to suggest that the total dV (both [retro]propulsive and from aerobraking) differs according to direction, and so a subway diagram of the Solar System needs two figures quoted for landings, at least for planets with a noticeable atmosphere.Looking at that map, why's the dV to get to the surface of Venus from low orbit so large (27 km/s) ? Now, yes, aerobraking would be of considerable benefit for Venus, but still, that diagram suggests that the total dV budget to land on Venus would be substantially more than to land on Mercury, which seems counter-intuitive.
Venus has an incredibly thick, dense atmosphere. That could be drag/gravity losses. You'll note that Earth is listed as 9.4km/s required, even though LEO energy is only ~8km/s. It could be an "adjusted" value accounting for the fact that ambient pressure makes rocket motors nearly useless on the Venusian surface.
A launcher of some sort (linear, or SpinLaunch-style) is a very large mass investment from the earth to the moon. However, once there the incremental cost of each kg of ice to orbit is essentially zero. That doesn't take into account the processing required to prepare the ice for transport. But a fully automated robotic facility could approach zero cost as well - if the lunar dust doesn't cut everything to shreds and force new hardware deliveries.Are you maybe somehow building those rockets out of Lunar regolith?Why would you take lunar ice to LEO, it is far less costly in money and delta v to launch the prop from Earth where it is far cheaper and you have more useful options.
Getting it to LEO from Earth isn't less costly, if you need five launches to refuel Starship, you're spending vast majority of your fuel for lift, not payload.
You do realize you don't have to process the water in the moon? Just ship it as it is, you can do the electrolysis in LEO as needed, as a bonus you don't have a 2 week night to deal with. Space(X) orbital gas station now open for business with low low cost on water, oxygen and hydrogen..
You see, to lift the water from the Moon you first need to get the rockets there somehow, meaning you launch them from Earth anyway, packed with fuel instead of water. Might need to refuel on LEO anyway. Then you use some of that fuel to land on the Moon and the rest of it launching again with the water, flying back to LEO and parking there. How is that supposed to be less costly than just lifting the water from Earth to LEO in the first place?
Oxygen and hydrogen are great and all, but their engine runs on methane.Getting it to LEO from Earth isn't less costly, if you need five launches to refuel Starship, you're spending vast majority of your fuel for lift, not payload.Why would you take lunar ice to LEO, it is far less costly in money and delta v to launch the prop from Earth where it is far cheaper and you have more useful options.
You do realize you don't have to process the water in the moon? Just ship it as it is, you can do the electrolysis in LEO as needed, as a bonus you don't have a 2 week night to deal with. Space(X) orbital gas station now open for business with low low cost on water, oxygen and hydrogen..
the most important number is cost, you need infrastructure that doesnt even exist yet on luna
Agreed. The infrastructure investment is huge hence talk of decades to set it up.
But having made that investment, the cost per ton of fuel delivered to LEO could be drastically, drastically lower. Cost of engines, cost of refurbishment due to aerodynamic damage, environmental cost of burned fuel, and so on.
I should add, I would be as delighted as anyone if instead in 50yrs time we're running fusion-powered atmospheric carbon capture operations to produce methalox etc. fuel here on Earth, with benefit of being virtually free and offsetting launch emissions (so who cares how many Starship launches it takes to fuel up in LEO). But any responsible power needs to be pushing all options at this stage, until one proves itself out ahead of the others.
Are you maybe somehow building those rockets out of Lunar regolith?
You see, to lift the water from the Moon you first need to get the rockets there somehow, meaning you launch them from Earth anyway, packed with fuel instead of water. Might need to refuel on LEO anyway. Then you use some of that fuel to land on the Moon and the rest of it launching again with the water, flying back to LEO and parking there. How is that supposed to be less costly than just lifting the water from Earth to LEO in the first place?
Not sure how great hydrogen is, for prop transfer type work, it doesn't like to stay liquid and it leaks through almost anything.Oxygen and hydrogen are great and all, but their engine runs on methane.Getting it to LEO from Earth isn't less costly, if you need five launches to refuel Starship, you're spending vast majority of your fuel for lift, not payload.Why would you take lunar ice to LEO, it is far less costly in money and delta v to launch the prop from Earth where it is far cheaper and you have more useful options.
You do realize you don't have to process the water in the moon? Just ship it as it is, you can do the electrolysis in LEO as needed, as a bonus you don't have a 2 week night to deal with. Space(X) orbital gas station now open for business with low low cost on water, oxygen and hydrogen..
EXPECTATION. What happens later, happens later. Also eh..... Airbus taking massive loss on 25 billion on complex expensive aerospace project.... That should be re-assuring to SpaceX, that these complex and costly aerospace projects always return profit..... Also Airbus is way bigger conglomerate, that can handle 25 billion of unexpected loss. what are SpaceXs cash reserves to write down to accounting (just lost 50 billion dollars on a Mars mission, no body seem to be willing to buy extra missions.
Why would you take lunar ice to LEO, it is far less costly in money and delta v to launch the prop from Earth where it is far cheaper and you have more useful options.
Getting it to LEO from Earth isn't less costly, if you need five launches to refuel Starship, you're spending vast majority of your fuel for lift, not payload.
You do realize you don't have to process the water in the moon? Just ship it as it is, you can do the electrolysis in LEO as needed, as a bonus you don't have a 2 week night to deal with. Space(X) orbital gas station now open for business with low low cost on water, oxygen and hydrogen..
The whole point of Starship is to make launch cheap, cost of a launch is just fuel (couple million) and operations (another few million) plus whatever margin SpaceX wants on it,
Are you maybe somehow building those rockets out of Lunar regolith?Why would you take lunar ice to LEO, it is far less costly in money and delta v to launch the prop from Earth where it is far cheaper and you have more useful options.
Getting it to LEO from Earth isn't less costly, if you need five launches to refuel Starship, you're spending vast majority of your fuel for lift, not payload.
You do realize you don't have to process the water in the moon? Just ship it as it is, you can do the electrolysis in LEO as needed, as a bonus you don't have a 2 week night to deal with. Space(X) orbital gas station now open for business with low low cost on water, oxygen and hydrogen..
You see, to lift the water from the Moon you first need to get the rockets there somehow, meaning you launch them from Earth anyway, packed with fuel instead of water. Might need to refuel on LEO anyway. Then you use some of that fuel to land on the Moon and the rest of it launching again with the water, flying back to LEO and parking there. How is that supposed to be less costly than just lifting the water from Earth to LEO in the first place?
NASA can dump 50 billion to Mars mission and say "We will never see that money back, but this isn't about profit". SpaceX is about profit. As much as Elon talks about grand plans for benefit of human kind, to operate SpaceX needs profit. It doesn't have tax payer base, that can fund missions as completely cost and loss missions.