Author Topic: Orion Discussion Thread 2  (Read 560343 times)

Offline pochimax

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Re: Orion Discussion Thread 2
« Reply #860 on: 10/02/2025 08:29 pm »
I am unclear on how commercial Orion could be made cheap enough to compete with Dragon for LEO missions, even with a different LV.

Because it is not for LEO  ;D

(Beyond Earth Orbit...)

« Last Edit: 10/02/2025 08:29 pm by pochimax »

Offline Proponent

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Re: Orion Discussion Thread 2
« Reply #861 on: 10/03/2025 09:09 am »
But it's not hard to imagine that modifying Dragon 2 for BEO use might be cheaper than using Orion. Recall the initial configuration of Dear Moon.
« Last Edit: 10/03/2025 09:09 am by Proponent »

Offline Proponent

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Re: Orion Discussion Thread 2
« Reply #862 on: 10/03/2025 09:38 am »
The whole thing smells to me like an oldspace marketing gimmick. Remember, for example, the unsubstantiated claims circa 2010 that commercial Shuttle operations were viable? The claims that that there was going to be non-NASA demand for Ares V and SLS? Lockheed benefits from the publicity, regardless of how remote the project's prospects.

I do not mean to cast any aspersions on BioAstro or suggest that its research projects are unworthy. But there is no hint as to who would pony up a billion or so bucks for this. The cash certainly won't come from BioAstro, a small nonprofit.
« Last Edit: 10/03/2025 09:38 am by Proponent »

Offline hektor

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Re: Orion Discussion Thread 2
« Reply #863 on: 10/03/2025 06:21 pm »
Sounds more like Axiom to me. It began with a few millionaires (Axiom 1), but soon shifted to countries—Saudi Arabia, Italy, India, and others. There’s clearly a market for wealthy nations eager to send their citizens to the Moon. Countries like the UAE or India could certainly afford it.
« Last Edit: 10/03/2025 06:23 pm by hektor »

Offline pochimax

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Re: Orion Discussion Thread 2
« Reply #864 on: 10/04/2025 07:11 am »
Sounds more like Axiom to me. It began with a few millionaires (Axiom 1), but soon shifted to countries—Saudi Arabia, Italy, India, and others. There’s clearly a market for wealthy nations eager to send their citizens to the Moon. Countries like the UAE or India could certainly afford it.

In addition, international agencies can contribute to the manufacturing and/or launch of the booster stage

Offline hektor

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Re: Orion Discussion Thread 2
« Reply #865 on: 10/04/2025 07:38 am »
The European Space Agency (ESA) can contribute by providing European Service Modules (ESMs) as in-kind payment. ESA, along with other agencies like JAXA or ISRO, could also offer launch services, such as the H3 rocket or its Heavy variant, or even supply a booster stage for the Orion stack to enable Trans-Lunar Injection (TLI).

« Last Edit: 10/04/2025 07:41 am by hektor »

Offline TrevorMonty

Re: Orion Discussion Thread 2
« Reply #866 on: 10/05/2025 12:25 am »
Dual launch with 2x Vulcan or 1x Vulcan (Orion +crew) +1x NG.  There 2 options for 2nd LV either send up fully fuel departure stage and rendezvous with Orion and crew or tanker to refuel Orion Centuar.

Not sure if Vulcan has performance to deliver Orion to orbit with LAS. Vulcan would be easiest LV to pair Orion with. ULA human rated SLS US and Atlas.

Offline hektor

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Re: Orion Discussion Thread 2
« Reply #867 on: 10/05/2025 07:33 am »
What is the minimum duration between two successive Vulcan launches ?

Offline pochimax

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Re: Orion Discussion Thread 2
« Reply #868 on: 10/05/2025 08:24 am »
It would be interesting to know the orbit in which each of the three rockets (Vulcan, NG, FH) would leave the spacecraft and to know what the booster stage would need to be to take the spacecraft to its target (NRHO) or even to other, closer lunar orbits. It would also be interesting to know whether the spacecraft could be launched with a more powerful service module.
Knowing the characteristics of the booster stage could give us clues about which current and future rockets (internationally, I mean) could launch it.

I understand that the spacecraft will always be launched from US soil and with US rockets, but the booster stage could be launched with international collaboration.

In my opinion, if this ever happens, it would happen this way from the very beginning. In other words, we would never see a mission of this type with 100% North American components.

The big question is whether an Ariane 64 would be sufficient, or if a more powerful rocket is needed, and then Europe and/or Japan would have to limit themselves to manufacturing the booster stage.

Offline Robotbeat

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Re: Orion Discussion Thread 2
« Reply #869 on: 10/06/2025 10:05 pm »
The announcement above is beyond the scope of the NASA Artemis project. Discussing how this new use of the Orion, what service module will support it, and what launch vehicle will be used to lift it to LEO and make this venture profitable may be beyond the scope of this "Beyond-LEO HSF - Constellation" thread.

If you want, I could create a new thread in the commercial section of the forum. Let me know.

Tony

It is the "Orion and Exploration vehicles" section in the Beyond-LEO HSF subforum, for a crewed circumlunar mission utilizing Orion. Why wouldn't it be a good fit here? The rest of the Commercial section mostly, if not entirely, deals with launchers, some unmanned (mostly LEO) spacecraft, and a few crewed LEO initiatives...
it’s suited for the commercial section it’s commercial.
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Offline StraumliBlight

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Re: Orion Discussion Thread 2
« Reply #870 on: 10/07/2025 01:43 pm »


Interview with Tony Byers, Program Director for Orion Services:

Quote
[5:40] "We want to be launching multiple times per year".
[5:50] Other sovereign nations can purchase the service.
[6:20] Aiming to fly Orion for the next 2 decades.
[7:00] Exploring all launch providers, including Europe.
[7:20] "I'm not at liberty to say which ones yet but there are multiple launch vehicles that can perform the job."
[7:40] Discusses using a transfer stage to the Moon for non SLS missions.
[8:30] Looking at scenarios that use refuelling and storable propellants.

Offline DanClemmensen

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Re: Orion Discussion Thread 2
« Reply #871 on: 10/07/2025 02:34 pm »
What is the minimum duration between two successive Vulcan launches ?
Information from public sources, (miss)interpreted by me:

ULA is nearing completion of the second VIF SLC-41, including a second Vulcan mobile launcher platform. This means they can stack two Vulcans in parallel, so they can probably launch them in quick succession (hours, maybe) but not on the same launch opportunity on one day. with only the one pad, they are constrained by the propellant load time and probably a bunch of things I'm overlooking. They cannot launch a third Vulcan from SLC-41 in quick succession.

They are also working on SLC-3 at Vandenberg, but to use it in a coordinated launch campaign with SLC-41, the orbit needs to be at a high inclination.

Offline hektor

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Re: Orion Discussion Thread 2
« Reply #872 on: 10/07/2025 03:00 pm »


Interview with Tony Byers, Program Director for Orion Services:

 

Thanks. Too bad the guy did not ask about the Service Module, because I would love to know Lockheed plans about that part.

Online catdlr

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Re: Orion Discussion Thread 2
« Reply #873 on: 10/07/2025 03:09 pm »
What is the minimum duration between two successive Vulcan launches ?
Information from public sources, (miss)interpreted by me:

ULA is nearing completion of the second VIF SLC-41, including a second Vulcan mobile launcher platform. This means they can stack two Vulcans in parallel, so they can probably launch them in quick succession (hours, maybe) but not on the same launch opportunity on one day. with only the one pad, they are constrained by the propellant load time and probably a bunch of things I'm overlooking. They cannot launch a third Vulcan from SLC-41 in quick succession.

They are also working on SLC-3 at Vandenberg, but to use it in a coordinated launch campaign with SLC-41, the orbit needs to be at a high inclination.

Stay up-to-date with the construction and modifications on this webpage, which is updated as progress continues. Note that SLC-3 is included, making it a bit messy to view all their changes. They also don't date each update. It latest is at the top and goes back in time as you scroll down.

https://blog.ulalaunch.com/blog/vulcan-infrastructure-modifications

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Offline hektor

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Re: Orion Discussion Thread 2
« Reply #874 on: 10/15/2025 07:52 am »
Excerpt from Exploration spatiale : comment l'Europe souhaite s'émanciper des États-Unis

Quote
He also plans to request funding for the sixth European Service Module (ESM 6). While modules 4 and 5 will serve as Europe’s contribution to Gateway, the sixth will compensate ESA for past benefits from the International Space Station (ISS). “If we want to be a reliable partner, we must deliver ESM 6,” he said. However, ESA has not yet signed contracts for ESM 7–9, pending firm guarantees of benefits for Europe. Without such assurances from the U.S., Neuenschwander wants to repurpose the ESM for future European missions.

Offline Coastal Ron

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Re: Orion Discussion Thread 2
« Reply #875 on: 10/16/2025 03:22 am »
Well, this is interesting:

Once unthinkable, NASA and Lockheed now consider launching Orion on other rockets - Ars Technica

Relevant quote:
Quote
...
It appears that the joint venture to commercialize the SLS rocket is defunct. Moreover, there are no plans to modify the rocket for reuse.

This appears to be one reason Lockheed is exploring alternative launch vehicles for Orion. If the spacecraft is going to be competitive on price, it needs a rocket that does not cost in excess of $2 billion per launch.

More tidbits in the article, including what Lockheed Martin is doing to make the Orion MPCV "reusable". Though what they call "reusable" really seems more like "salvageable & refurbish- able" across three ships, and of course the Service Module is non-recoverable.

Still, interesting to see what they are trying to do, even though my opinion is that the Orion represents the end of an evolutionary line of capsule spacecraft, and that we would be better off putting our money into building the next generation of fully reusable space-only vehicles.
If we don't continuously lower the cost to access space, how are we ever going to afford to expand humanity out into space?

Offline DanClemmensen

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Re: Orion Discussion Thread 2
« Reply #876 on: 10/16/2025 03:37 am »
Well, this is interesting:

Once unthinkable, NASA and Lockheed now consider launching Orion on other rockets - Ars Technica

Still, interesting to see what they are trying to do, even though my opinion is that the Orion represents the end of an evolutionary line of capsule spacecraft, and that we would be better off putting our money into building the next generation of fully reusable space-only vehicles.
After reading the article I don't think it's "what they are trying to do". I think it's what their upper management and business development folks are trying to pitch to NASA. I strongly suspect this will go absolutely nowhere, just like "commercialized SLS" in 2022.

Online Vultur

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Re: Orion Discussion Thread 2
« Reply #877 on: 10/16/2025 03:43 am »
Still, interesting to see what they are trying to do, even though my opinion is that the Orion represents the end of an evolutionary line of capsule spacecraft, and that we would be better off putting our money into building the next generation of fully reusable space-only vehicles.

I don't think the problem with Orion is that it's a capsule. Capsules are fine. The problems with it are the "old space"/legacy contractor/cost plus model, and scaling issues from 'scaling up Apollo'.

I am not sure we should be putting "our" money (if by that you mean US government development money) into new government-specified "conventional" HSF hardware at all. I think SpaceX, Blue, Vast, Axiom, etc can do that perfectly well. I'd rather see that money go to things that the private companies can't realistically do, like nuclear development, or things that are pretty unknown but could be massively useful if they work, like Wind Rider/plasma magnet/magnetic sail/electric sail type systems or how to deploy/unfold really large solar sails or enormous areas of very thin film solar panel in space.

(This is why I'm not as negative on Gateway as some ... PPE at least represents a human-rated SEP system with much higher power & thrust than has been flown before, whereas SLS and Orion really do nothing new at all.)

Offline hektor

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Re: Orion Discussion Thread 2
« Reply #878 on: 10/16/2025 11:15 am »
If ESA does not sign for ESM 7–9, I am sure that US Industry can build a substitute (maybe more capable, like LLO compatible), but how long would it take ?
« Last Edit: 10/16/2025 11:16 am by hektor »

Offline StraumliBlight

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Re: Orion Discussion Thread 2
« Reply #879 on: 10/16/2025 01:48 pm »
Well, this is interesting:

Once unthinkable, NASA and Lockheed now consider launching Orion on other rockets - Ars Technica

Quote
Wanted: a heavy lift rocket
This appears to be one reason Lockheed is exploring alternative launch vehicles for Orion. If the spacecraft is going to be competitive on price, it needs a rocket that does not cost in excess of $2 billion per launch.

Orion has a launch mass, including its abort system, of 35 metric tons. The company has looked at rockets that could launch that much mass and boost it to the Moon, as well as alternatives that might see one rocket launch Orion, and another provide a tug vehicle to push it out to the Moon. So far, the company has not advanced to performing detailed studies of vibrations, acoustics, thermal loads, and other assessments of compatibility, said Kirk Shireman, Lockheed Martin’s vice president and program manager for Orion.

[...]

Orion is always going to be relatively expensive. However, officials said they are on track to trim the cost of producing an Orion by 50 percent from the Artemis II to Artemis V vehicles and in follow-on missions to bring this down by 30 percent further or more. Minimizing refurbishment will be key to this.
« Last Edit: 11/19/2025 05:55 pm by StraumliBlight »

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