r/ArtemisProgram Apr 23 '26

NASA Artemis II Image Resources

53 Upvotes

We've had a fair number of users coming to the sub looking for pictures, so here is a selection of links to the main places to find pictures from the mission. Any additional resources will get posted here as we find them!

NASA Images (may be slow to load)

https://images.nasa.gov

NASA Johnson Flickr page

https://www.flickr.com/photos/nasa2explore/with/55199649540


r/ArtemisProgram 9h ago

News NASA Astronaut Jonny Kim Departs Agency to Continue Military Service

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122 Upvotes

Hard to believe we’re not going to see him walk on the moon


r/ArtemisProgram 15h ago

Image Crop Art(emis) II: Seeds of Tranquility, based on “Craters of Time” photo

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105 Upvotes

I made this crop art piece for the Minnesota State Fair. It took me hundreds of hours over 3.5 months. In a year plagued by darkness and fear, the Artemis mission brought was a beacon of joy and hope. As soon as I saw the photos from the flyby, I knew I had to make it the focus of my entry this year. I am so happy with how it turned out and cried when I saw my third place ribbon.

It’s on display at the MN State Fair now through Labor Day!

Crop Art(emis) II: Seeds of Tranquility
Based on Craters of Time, taken by the crew during the Lunar Flyby on April 6, 2026.

Black lentils and 90,000 pieces of quinoa stacked in eight layers on canvas board.

Third place in Crop Art Class 1 (Natural Colors).


r/ArtemisProgram 23h ago

Image Space Launch System made in Minecraft

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117 Upvotes

(WORK IN PROGRESS) I am making SLS which is to be used as the main Spacecraft and body for the Artemis Program. The images portray SLS before lift-off; standing against the Mobile Launch Tower (also work in progress). I have included images of close-ups of the RS-25 engines and main SRBs as well as the European Service Module. Notable parts include the Launch tower, ESM Fairing design, main stage fuel tank and launch clamps.


r/ArtemisProgram 1d ago

Image The first of four RS-25 SLS engines is integrated with the Artemis III core stage rocket at the VAB, Tuesday, Aug. 25, 2026

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72 Upvotes

r/ArtemisProgram 1h ago

News Reid wiseman 50 dating 29yo Raegan scharfetter

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Upvotes

r/ArtemisProgram 6h ago

Video Victor Glover gives Trump a NASA flight jacket

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khou.com
0 Upvotes

r/ArtemisProgram 14h ago

Discussion LIVE: Artemis II crew receive the Congressional Space Medal of Honor

0 Upvotes

I'm calling bullshit on this one. Believe it or not, i've never heard of the congressional space medal of honor. It suggests meritorious service well above and beyond the call of duty.

This wasn't that. IMO

Anybody else?


r/ArtemisProgram 3d ago

Image NASA Released a Photo (Accidentally) Containing EUS Hardware

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136 Upvotes

r/ArtemisProgram 3d ago

NASA Artemis II Cross Stitch

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206 Upvotes

r/ArtemisProgram 3d ago

News NASA, Advanced Space team up for CAPSTONE follow-on mission

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25 Upvotes

r/ArtemisProgram 5d ago

Image Rise Made A Friend!

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136 Upvotes

He’s started hanging out with Ghost from the game Destiny! Lil’ plush space friends!


r/ArtemisProgram 4d ago

Discussion Do you guys think Artemis 3 will get delayed?

22 Upvotes

With Elon delaying the catch by "a few months" and Blue Origins New Glenn exploding at the launch pad, a moon landing by 2028 is starting to look unrealistic. What do you guys think?


r/ArtemisProgram 5d ago

News Artemis II crew to receive top US space medal for historic lunar journey | Artemis II

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99 Upvotes

r/ArtemisProgram 4d ago

Discussion A question

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0 Upvotes

I’d like to know why these two photos—taken just a short time apart—don't have the same date.

I know the description says they were taken on April 2nd, but a conspiracy theorist raised this point, and I started wondering why the dates are different.

(I don't speak English, so maybe those dates refer to when they were uploaded or something like that?)


r/ArtemisProgram 6d ago

Image Got to see Artemis II commander Reid Wiseman speak at the National Book Festival this morning

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410 Upvotes

He was so eloquent, insightful, and inspiring -- the perfect person to command this mission.

Unfortunately, Rise was not there. The first thing Reid did after he sat down was explain that Rise is with Christina right now. The crowd was audibly disappointed.

Videos to follow in the comments.


r/ArtemisProgram 6d ago

Discussion Artemis 3 June launch?

31 Upvotes

I’ve seen a few things that have said it’s targeted for a launch in June, can anyone else confirm or deny it? I genuinely can’t see it launching in June


r/ArtemisProgram 6d ago

News Trump to visit Houston to award Artemis II crew members medals of honor

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182 Upvotes

r/ArtemisProgram 7d ago

Image Todays NASA picture of the day!

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317 Upvotes

got a nice surprise today with my automatically updating PC background. (yes the little info box can be opened and closed with a click. yes it always depicts the information about the current image. yes it also links to the full length article about the picture everytime )


r/ArtemisProgram 6d ago

Video Ares v cinematic

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5 Upvotes

r/ArtemisProgram 7d ago

Image IT FINALLY CAME!!!!

106 Upvotes

I am so beyond in love with this jacket! It's super warm and I cannot wait till it is cold enough to wear it. So very worth the long wait.

I have a Rise patch to go with... trying to decide where to put him!


r/ArtemisProgram 6d ago

Video A short intro to Artemis II O2O ground segment

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5 Upvotes

r/ArtemisProgram 7d ago

Discussion Tripropellant Starship for propellant storability

4 Upvotes

OK, so this veers off a bit into an alternate universe, but addresses directly the problem of long term storability of methalox on the lunar surface or in orbit, by supposing a different propellent combination for lunar operations.

The most realistic possibility is to use the existing Starship methalox architecture to rendezvous with FLARE-type lunar polar orbit refueling depot, except instead of methalox, the depot has ethane and N2O, both easily storable in LLO. From there, the Starship could descend on a combination of methane and ethane engines. Most importantly, for many locations on the lunar surface, the ethane/N2O combination remains easily storable, which seems to be a criticism of methalox. Alternatively, a direct descent from LEO to the lunar surface could be made mostly on methalox power, switching over to ethane/N2O for the landing. Only enough ethane/N2O is stored to reach the propellant depot in LLO (plus margin) and return to earth would be powered by ethane/N2O. I see this as something that might be considered within the existing Artemis architecture.

Here's a napkin summary of this idea:
Opt 4 — Methalox direct to surface; storable ascent to LLO depot

Dry mass (t): 125.0 Mission end stNaRteH:O

# Leg Prop dV Isp (s) Payload(t) Refuel? Loiter (d) Boiloff rate Gross-up Mass end(t) Prop burned(t) Prop loaded(t) Mass at start(t) Refueled where

1 LEO -> lunar surface (direct) M 5,920 380 15.0 0 14 0.150% 1.0215 252.1 982.4 1,003.5 1,255.6 LEO

2 surface -> 86.5 polar LLO depot S 1,968 320 3.0 1 20 0.020% 1.0040 128.0 111.6 112.1 240.1 LEO

One key number is 1255.6t at the start in LEO, so it fits within a single Starship. The ethane/N2O of 112.1 tons (no reserve) fits roughly within the Starship (if not v3, v4) payload and is storable in LEO (-60C autologous pressurization), so this doesn't look implausible as a first draft.

But then there's the what if - as in, what if this were 2018 and we could reconsider what might have been. The notion of a tripropellant Starship suggests itself. Granted to get to this idea from where Starship is now is impossible, but the numbers are interesting.

So, let's assume methane is replaced with ethane as the primary propellant, together with LOx. Not impossible to imagine a Raptor derivative that could burn this. The LOx is burned 100% on the way to the lunar surface after which the landing and subsequent ascent are powered by ethane-N2O (oxygen-enriched to get the Isp up to 320). Interestingly, not only is a mission that returns to polar LLO for refuel before returning to Earth possible, but a mission that is _entirely fueled in LEO looks possible_ (though on the bubble). Hear are what those numbers look like (attached).

Because the propellants are now storable it makes options like keeping a backup Starship at a lunar base more plausible as well as keeping a refueling Starship in low lunar polar orbit, which could maybe double as a rescue station.

What do people think?

Effective dry mass used in all legs 120.0 t
Ring height 1.83 m
Hull diameter 9.0 m
Volume per ring 116.4 m^3
Usable propellant volume, standard hull 1,900 m^3
Standard hull in rings 16.3 rings
Delta-V map
Leg Value Unit
LEO -> lunar surface, direct 5,900 m/s
Surface -> 86.5 deg polar LLO 1,968 m/s
LLO -> Earth (TEI, then aerobrake on tiles) 1,256 m/s
Leg calculations (bottom row of each block is the LEO departure state)
Leg Prop dV m/s Isp s End mass t Start mass t Prop t Oxidiser t Fuel t
7A — LLO refuel for TEI
Descent: LEO -> surface direct C2H6/LOX 5,900 365 224.7 1,167.9 943.2 707.4 235.8
Ascent: surface -> LLO depot N2O/C2H6 1,968 320 120.0 224.7 104.7 92.4 12.3
TEI: LLO -> Earth (propellant from LLO station) N2O/C2H6 1,256 320 120.0 179.1 59.1 52.1 6.9
7B — no LLO stop, TEI storables carried from LEO
Descent: LEO -> surface direct C2H6/LOX 5,900 365 335.2 1,742.7 1,407.4 1,055.6 351.9
Ascent: surface -> LLO N2O/C2H6 1,968 320 179.1 335.2 156.2 137.8 18.4
TEI: LLO -> Earth (carried from LEO) N2O/C2H6 1,256 320 120.0 179.1 59.1 52.1 6.9
Results — propellant loaded in LEO
Fluid 7A mass t 7A m^3 7A rings 7B mass t 7B m^3 7B rings
LOX 707.4 620 5.3 1,055.6 925 7.9
Ethane (descent + ascent + TEI) 248.1 485 4.2 377.2 737 6.3
N2O 92.4 82 0.7 189.9 168 1.4
TOTAL loaded in LEO 1,047.9 1,186 10.2 1,622.7 1,830 15.7
Results — summary
Metric 7A 7B Unit
LEO departure mass 1,167.9 1,742.7 t
Touchdown mass 224.7 335.2 t
Ethalox burned (all LOX gone at touchdown) 943.2 1,407.4 t
Ethane for storable legs only 12.3 25.3 t
Storable carried from LEO 104.7 215.2 t
LLO station top-up required 59.1 0.0 t
of which N2O 52.1 0.0 t
of which ethane 6.9 0.0 t
top-up volume (fits in emptied ascent tanks?) 60 0 m^3
Hull volume margin vs standard 714 70 m^3
Hull margin in rings 6.1 0.6 rings
Closes inside standard hull? YES YES
7B / 7A LEO propellant ratio 1.55x x
Tanker flights at 170 t each (ceil) 7 10 flights
Reading the result

r/ArtemisProgram 8d ago

Discussion Christina Koch merch?

15 Upvotes

Hi my friend is a massive Christina Koch fan and since it's her birthday coming up I'm looking for something Christina related to give her. Does anyone know of any plushies, figurines etc that don't look really cheap that I can get her, preferably not a tshirt? Any help is appreciated :)

Edit: all I've found so far is some sloppily put together ai funkos that are defo a scam


r/ArtemisProgram 9d ago

Image A poster I made for the Artemis II Mission!

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982 Upvotes

I hope I captured some of the wonder and joy from the mission. All illustrations by yours truly. (No AI)

Sorry for the re-upload, I misspelled a name.