New Glenn Update
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Regulars are buzzing about Blue Origin's New Glenn rocket upgrade, touted to boost performance with enhanced BE-4 engines and subcooled components. Commenters riff on the implications of these upgrades, with some speculating about the potential for increased payload capacity and others pondering the challenges of implementing subcooled propellants. As enthusiasts dissect the details, a consensus emerges that New Glenn is shaping up to be a formidable competitor in the heavy-lift launch market. The excitement is palpable, with many eagerly anticipating the rocket's maiden voyage and the potential breakthroughs it could bring.
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Nov 20, 2025 at 4:21 PM EST
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I wonder how they'll be implementing that since SpaceX gave up on recapturing fairings (seemingly too soon, but only from the POV of someone with no internal info).
> SpaceX performs some amount of cleaning and refurbishing before using the previously flown fairings on a subsequent flight. SpaceX has reflown fairing halves more than 300 times, with one being reflown for 34 times.
They gave up on catching them in nets, because it turns out they're fine splashing directly into the water.
https://en.wikipedia.org/wiki/Blue_Moon_Pathfinder_Mission_1
I don't need a YT influencer to know my NASA history. I'm old enough it was taught in school while young enough to not have lived through any of it.
FYI, that talk was poorly received in the aerospace community.
Destin missed that the entire point of Artemis is not to one and done the Moon again but build towards getting to Mars. And the repeated "we're going, right?" shtick was condescending in the same way Hegseth wanting generals to cheer and holler for him was.
He acted like a petulant influencer. Not a science communicator.
Either way, your criticism of Destin's presentation hits. One and done'ing the Moon is not particularly helpful in setting up a sustainable cislunar economy.
In 2017 Space Policy Directive 1 amended the national space policy to pursue "the return of humans to the Moon for long-term exploration and utilization, followed by human missions to Mars and other destinations" [1]. This formally established the Artemis program [2].
Destin's criticisms were apt for Constellation [3], which was closer to an Apollo reboot. They were uninformed for Artemis.
[1] https://trumpwhitehouse.archives.gov/presidential-actions/pr...
[2] https://en.wikipedia.org/wiki/Artemis_program
[3] https://en.wikipedia.org/wiki/Constellation_program
Nevertheless, it's hard to imagine any kind of sustainability when each launch costs north of $2 Billion and nearly all hardware is thrown away each time. In that sense, his criticism was very valid, even if tough to hear.
I said aerospace community. Not NASA. Plenty of people hate Artemis. Most people hate SLS. But they hate it for good reason. Destin touched on some of that. But because he missed Artemis's purpose, he bungled that criticism too.
I like Destin. But he missed the mark pretty badly on that video, and I judge him for now following up with clarification.
NASA doesn't build rockets. ULA (Lockheed Martin + Boeing), Northrup Grumman, Aerojet Rocketdyne, etc. do. That's what I took "aerospace community" to mean. The community of people working in aerospace. Artemis has shifted focus several times now, since before it was called "Artemis" as each political administration has emphasized different goals, and as mission planning has evolved with hardware development. Over the years I have read everything from an abstract Moon-to-Mars testbed, a 5 year deadline crash program to land "the first woman and the next man" at the lunar south pole, a sustained lunar presence, the "first woman and first person of color" on the moon, safety science and Mars prep, and latest a de-scoping of the cis-lunar gateway station and shift toward private industry. Such things are difficult to avoid under constantly changing leadership.
Given that, I don't see any problem with the way Dustin presented the situation, nor do I feel any kind of need for an apology or clarification.
The factory tours for the two show this difference. New Glenn production is a lot more classical aerospace in terms of a high tech cleanroom factory being built from the start, versus a rocket that started out being built in tents that is slowly guiding the factory design as the tolerances are sorted out.
I think Blue's philosophy is pretty similar to the old space giants, except for being willing to invest a ton of money into improvements and new technologies without waiting around for the government to give them a blank check first.
Maybe we'll find that the thing limiting aerospace progress wasn't even that old space was afraid to test, but rather that they were simply unwilling to progress on their own initiative.
The third flight of the Saturn V took 3 astronauts in their spacecraft to lunar orbit and back.
https://appel.nasa.gov/2010/02/25/ao_1-7_f_snapshot-html/
Human spaceflight is more about mitigating risk than anything. Apollo was getting there first, so there was a willingness to take more risks.
Also, NASA at the time had a humongous budget compared to today, adjusted for inflation [1] and it was a lot more focused on just getting to the moon.
1: https://en.wikipedia.org/wiki/Budget_of_NASA
News at 10
FYP as it's rather worse than you framed. I'm happy to see more competition in space, because I think it's the single most important domain for humanity. And Blue Origin is making some rapid improvements, but people are dramatically overstating both this and their history/role in space quite significantly.
Blue Origin was founded before SpaceX, back in 2000, and only managed to send a rocket into orbit this year, 25 years later. They remain a complete nonplayer that exists only through the good fortune of endless and clearly unconditional Bezos bucks.
Now if they can keep putting out some good results, ideally start producing some hardware that can compete in terms of price and capability, and generally scaling things up - then I'll be the first to sing their praises. But we're still quite a ways away from that point for now.
Additionally, the New Glenn fairings are very large for their weight capacity. New Glenn has 3x the fairing volume compared to the Falcon Heavy, but can throw less mass. So many expected that BO designed it this way because they expected to increase performance of their engines in the future, making the weight/volume ratio of their fairing more balanced.
New Glenn has 45t of capacity now. Increasing thrust by 15% should increase that to 51t, thus making New Glenn 7x2 also just barely a Super Heavy booster. Perhaps they didn't call that out because that would overshadow the 9x4 announcement.
To be fair, the Falcon Heavy has way too little fairing volume for it's lift capacity (and apparently it is in the process of getting an extra 50% or so?)
The small size of the Falcon Heavy fairing is probably due to the fact that they are the same size as the Falcon fairing, and it was designed when Falcon could throw < 1/2 the mass it can currently throw, let alone the Falcon Heavy.
BE-4 is 140 bar chamber pressure vs SpaceX Raptor 2 at 350 bar. Thrust to weight of BE-4 is 80:1 vs Raptor2 at 140:1.
I don't think the capabilities are as different as those numbers imply. I believe that it's due to the conservativeness of Blue Origin and SpaceX's willingness to blow up hundreds of engines on the test stand to iteratively push the margins.
BE-4's chamber pressure is low for its design, but it would be very difficult to increase it to Raptor's levels. Full-flow staged combustion causes the propellants to be gasses when they enter the combustion chamber, and chemical reactions in gasses happen more quickly, allowing for efficient combustion in a smaller combustion chamber. The smaller volume makes it easier to contain higher pressures.
Increasing thrust by 15% doesn't just increase payload by 15%. I don't know a simpler way to estimate this than to run a simulation, and I don't have one with numbers I can toggle.
Blue Origin is matching from Raptor 2 to Raptor 3. Comparing thrust at sea level, lbf:
Raptor 2 | 507,000 [1]
Raptor 3 | 617,000 [1]
BE-4 | 557,143
BE-4' | 642,857
BE-3U | 160,000
BE-3U' | 200,000
[1] https://en.wikipedia.org/wiki/Ton-force#Tonne-force
What does it mean?
On a funnier note, the 9 in Falcon 9 is the number of engines. So blue origin is somewhat picking up on their naming scheme. Or, by BO's scheme, it'd be the Falcon 9x1, or the Starship 33x6.
...and we'd be back to steam engine wheel formulas: https://en.wikipedia.org/wiki/Whyte_notation
Ignoring that weaponizing space would backfire badly (you want hundreds of nukes in orbit? yeah actually let's just not do that) and thus no one considering it either.
But miles has gone out of fashion. Pounds too..
After all, they’re the ones manufacturing the imperial screws, etc.
Likewise, Liberia set up a transition program in 2018.
AFAIU both still use a bunch of traditional non US units too, like the UK.
Can someone from the industry confirm whether they use metric internally and the stream uses imperial just for the patriotic show or whether imperial units are used because some countries use different unit systems and this is normal?
On a related note, I don't think anyone is bothered buying screens (monitor/phone/...) labeled in inches, but orbital elevations and speeds? Weird.
Considering all these, you'd expect space sector to borrow from the aviation sector. But we use SI systems exclusively. Everything in metres, kilograms, seconds. Feet, miles, knots etc are unheard of (Well, we have heard of them. We just don't use them). SI units make calculations and our life a magnitude of order easier. I need to check up how it is with winged reentry vehicles. But they're also likely go with m/s rather than knots. The only time we face difficulty with esoteric units are when we use some rare sensors. You end up looking up the definition of 'BTU' and other similar atrocities.
There are two noteworthy exceptions to this trend though. It's when specifying engine thrust and specific impulse. Engine thrust is often specified in kilograms, (metric) tonnes etc. Of course they mean kgf and Tf (weight equivalent of that mass under 1g). Meanwhile mN, N, kN and MN are also used equally frequently. It's a perennial source of frustration and conflict, with younger generation preferring SI units and the seniors preferring kilograms and tonnes. Meanwhile, specific impulse is even weirder. If you were using SI units, you'd expect N.s/kg or m/s or something similar. Even if you were using imperial units, you'd expect something similar. But the unit everyone actually uses is seconds. For examples, a high end cryogenic engine may deliver an Isp in the range of 450s (SSME had a vacuum Isp of 452s). Sometimes, it's also expressed as 'effective velocity' of exhaust in m/s. There are logical explanations for all these weird units. But the reality is that none of them, including the SI units are strictly correct, because they all use some sort of scaling that isn't linear or an assumption that doesn't apply.
You can blame the US for all these inconsistencies in the space sector. The Americans have a habit of making up units on the spot. For example, the kT, MT yields of nukes were invented by the Manhattan project scientists. Similarly, the unit of nuclear criticality is dollars and cents - thanks to Louis Slotin. (Sadly, he passed away soon after the second criticality accident with the demon core). Anyway, the US also has shot themselves in the foot by mixing up units. The Mars Climate Orbiter crashed into the planet instead of entering its orbit due to the engineers mixing up the SI and imperial units. Moral of the story, if you plan to go to space, you better choose a measurement system and stick to it. Also, don't make a round scrubber for the command unit and a square scrubber for the lander. Make up your mind first!!
Some things are ridiculously better in the imperial system - like temperature: In Fahrenheit, 0 is roughly the coldest mean day in densely inhabited areas, and 100 is the hottest. In Metric, 0 is the freezing point of water at sea level in ambient temperatures and with a low barometer reading, 100 is boiling in the same conditions.
Since I measure weather much more frequently than I measure water temps, I am driven cukoo by the silly Centigrade system.
Also, The splitting into 12 used by the foot is more useful, in my experience, than the ten of the metric. In fact, I strongly decry that we teach our kids to use base 10 instead of the much more efficient and easier to divde into fractions of base 12. (You can teach kids to count joints on thier fingers [using the thumb as a pointer] to get to 12x12 on two hands, and give the kids a headstart on fractions, multiplication and division, but I digress..)
On the other hand, having both an Imperial Gallon and a US Gallon, etc, where the same word is used for different amounts, now THAT is insane.
But then I grew up with Celsius, so no wonder I'm used to it!
As someone who grew up with metric, my opinion is that nothing that imperial people claim is unintuitive with metric is, in fact, unintuitive to me. Nothing. And I tried hard. We're used to what we're used to :-).
> Some things are ridiculously better in the imperial system - like temperature
This says that you grew up with imperial, I'm convinced of it!
> In fact, I strongly decry that we teach our kids to use base 10 instead of the much more efficient and easier to divde into fractions of base 12.
What's the argument there? That because you can divide 12 by 2, 3, 4 makes it vastly easier than 10, because 10 you can only divide by 2 and 5? How does that make it easier to learn fractions? What about the fact that in metric, a centimeter is 1/100 of a meter, and a millimeter is 1/1000 of a meter? Those are fractions, right?
Just to make it clear: I am not claiming anything about imperial being ridiculous; I totally understand that if you grew up with it, then it's intuitive to you. What I don't understand, really, is all those imperial people who just cannot seem to apprehend the idea that maybe, just maybe, they are biased because imperial is what they know better. Is it that hard? It makes me concerned about cultural differences... do those people realise that others may have different cultures, and that it is okay and not ridiculous?
PS: I upvoted you because I don't find it fair that you get so many downvotes for an innocent opinion. I don't share your opinion, but it's not offensive or anything like that :-).
Everybody hates swapping between units of measurement. You pick one and stick with it. It's natural having the need to move between two measurement systems irritates you.
>I measure weather much more frequently than I measure water temps,
In cold climates water temp is actually the most important thing to know about the weather by a long shot. The freezing point tells you if it's wet or dry, slippery or non-slippery.
Also feet happen to be the standard measurement of altitude in aviation, which rockets are part of, even in metric countries, I hate it but it's like that. Distances are nautical miles, a not so bad unit (it corresponds to 1 arcminute on earth), which make me hate the use of terrestrial miles in articles partaking to aviation even more. But it is a bit offtopic here because most of the article is metric.
It sounds as if they already have a long line of customers which have booked flights to all these destinations. (If they actually do, splendid!)
These expected and incremental updates (to a years late system that still needs to be proven) are putting the payload capacity in the Falcon Heavy range and there's roughly 1 Falcon Heavy launch per year.
There are over 100 Falcon 9 launches per year. Yes a bunch are Starlink so you can exclude those when estimating demand from external customers but the point remains that there isn't currently a commercial demand for bigger payloads and/or higher orbits than what Falcon 9 can do.
SpaceX has the same problem: Starship is a superheavy lifter where Falcon Heavy has little demand and Starship is even bigger. At least SpaceX has Starlink as induced demand. Blue Origin doesn't.
Defenders will argue the greater volume and payload weights will create new possibilities because payloads can only be designed for available launch systems but satellites don't really seem to be getting any bigger and there are only so many geosynchronous military payloadcs and interplanetary probes that need to be launched.
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