Did Artemis I Miss the Moon? | |
RestoreTheAnger
User ID: 78146701 United States 11/27/2022 02:17 PM Report Abusive Post Report Copyright Violation | |
BrainGuy, MAGA Republican
White heteropatriarchal supremacist chemophob User ID: 84804751 United States 11/27/2022 02:27 PM Report Abusive Post Report Copyright Violation | Space is flat. The moon is a hologram. And Joe Biden is president. Last Edited by BrainGuy: Q* on 11/27/2022 02:29 PM --------------- Don't care. Still voting Trump! ---------- |
Stumpknocker
User ID: 83868295 United States 11/27/2022 02:30 PM Report Abusive Post Report Copyright Violation | |
Bean223
User ID: 83318340 United States 11/27/2022 02:34 PM Report Abusive Post Report Copyright Violation | |
Astromut
(OP) Senior Forum Moderator 11/27/2022 02:35 PM Report Abusive Post Report Copyright Violation | |
Bean223
User ID: 83318340 United States 11/27/2022 02:39 PM Report Abusive Post Report Copyright Violation | People actually think a rocket launched from Earth GOES STRAIGHT UP to the Moon...... Quoting: Bean223 Sadly, yes. Even the spectator next to my telescope was all confused when it "went past the moon." You know I'm no astronomer or expert in rocketry or spatial navigation. I literally learned enough from watching old 1960s Disney reruns about the space program, along with 90s discovery channel to know wtf is going on. It's shocking how little people learn today. Of course Disney is more worried about being woke. And who knows wtf is on discovery channel these days....I dont watch tv. Last Edited by Bean223 on 11/27/2022 02:40 PM |
91GMC
User ID: 75967661 United States 11/27/2022 02:59 PM Report Abusive Post Report Copyright Violation | |
BrainGuy, MAGA Republican
White heteropatriarchal supremacist chemophob User ID: 84804751 United States 11/27/2022 03:33 PM Report Abusive Post Report Copyright Violation | People actually think a rocket launched from Earth GOES STRAIGHT UP to the Moon...... Quoting: Bean223 Sadly, yes. Even the spectator next to my telescope was all confused when it "went past the moon." You know I'm no astronomer or expert in rocketry or spatial navigation. I literally learned enough from watching old 1960s Disney reruns about the space program, along with 90s discovery channel to know wtf is going on. It's shocking how little people learn today. Of course Disney is more worried about being woke. And who knows wtf is on discovery channel these days....I dont watch tv. Children are taught how to put a condom on a "woman" on May Day now. --------------- Don't care. Still voting Trump! ---------- |
BrainGuy, MAGA Republican
White heteropatriarchal supremacist chemophob User ID: 84804751 United States 11/27/2022 03:35 PM Report Abusive Post Report Copyright Violation | |
Buck Fiden
User ID: 84257938 United States 11/27/2022 04:30 PM Report Abusive Post Report Copyright Violation | |
G3
User ID: 84495720 United States 11/27/2022 04:39 PM Report Abusive Post Report Copyright Violation | |
BrainGuy, MAGA Republican
White heteropatriarchal supremacist chemophob User ID: 84804751 United States 11/27/2022 04:50 PM Report Abusive Post Report Copyright Violation | Quoting: G3 I would pay real money to see "TILT" light up in his eyes when that happens. --------------- Don't care. Still voting Trump! ---------- |
scimitar
User ID: 77713000 United States 11/27/2022 05:05 PM Report Abusive Post Report Copyright Violation | Astro... I have a question for you. Are they just playing orbital mechanics games to conserve fuel? I mean 6 days to the moon, correct me if I'm wrong but didn't the Apollo missions only take 3 days? To me it seems like they started from scratch for this mission... how long did it take from the initiation of this program? Perhaps this is what happens when NASA is on an un-expandable budget. From a technical standpoint you are clearly in the top 10% of all GLP posters... Remember Idol Harobed? (Deborah Lodi), those were the days... doing battle with IDW (Inter Dimensional Warrior). Ominous regressions One Truth... many realities |
777light
User ID: 78218847 United States 11/27/2022 05:15 PM Report Abusive Post Report Copyright Violation | |
Astromut
(OP) Senior Forum Moderator 11/27/2022 05:21 PM Report Abusive Post Report Copyright Violation | Astro... I have a question for you. Quoting: scimitar Are they just playing orbital mechanics games to conserve fuel? I mean 6 days to the moon, correct me if I'm wrong but didn't the Apollo missions only take 3 days? To me it seems like they started from scratch for this mission... how long did it take from the initiation of this program? Perhaps this is what happens when NASA is on an un-expandable budget. From a technical standpoint you are clearly in the top 10% of all GLP posters... Remember Idol Harobed? (Deborah Lodi), those were the days... doing battle with IDW (Inter Dimensional Warrior). IDW is still around here, he just doesn't use his screen name because he knows he's ban on sight. He likes to make threats and such to this day. Anyway, to get to the meat of your question, yes the trajectory here is very different. SLS is a very different animal than the Saturn V, though both are super heavy lift. Saturn V had three stages, SLS has two solid boosters, a large core stage and at the moment a small "interim" upper stage. The Orion's service module does not have as much fuel and delta-V as the Apollo CSM had. To give you an idea, the Apollo CSM carried about 18,410 kg of propellant for the main SPS engine and the Apollo command module was a smaller capsule than Orion. Orion's European Service Module only has a propellant mass of about 8,600 kg and carries a heavier capsule. Ironically, both the CSM and European Service Module rely on versions of the AJ-10 engine, though Orion's is literally an old Space Shuttle OMS engine that has been repurposed for one more flight. Orion with its current service module cannot perform the mission profiles that Apollo's CSM could. It can't carry a lander into low lunar orbit and then get itself out of low lunar orbit for a return to earth. Likewise, the ICPS is very under-powered compared to the mighty Saturn V upper stage, the S-IVB. The ICPS is really just a modified Delta upper stage, and it only carries about 28,576 kg of propellant mass vs 109,000 kg for the S-IVB. The upgraded Exploration Upper Stage or EUS will flip that statistic later on, but for now the ICPS is what Orion had to work with. Given these limitations and the nature of the SLS rocket's staging, the core stage put Orion and the ICPS into a slightly elliptical parking orbit that essentially gave the ICPS a "head-start" before the TLI burn (on the Saturn V, the S-IVB finished the orbit insertion itself and stayed in a low parking orbit until TLI). Even so, the ICPS and Orion cannot fly the kind of profile we saw with Apollo, so they opted for an easier but slower trajectory to a distant retrograde orbit of the moon, swinging wide past the moon each time and never braking fully into a low lunar orbit. This is similar to how later missions will utilize a halo orbit that stays farther from the moon than Apollo and a lunar lander that will meet Orion there and depart to the surface from a wider starting orbit. This trajectory does not require as much delta-V from Orion to do the mission and still get back to earth. Last Edited by Astromut on 11/27/2022 05:23 PM |
Mr. Chimpington
User ID: 84704393 United States 11/27/2022 05:28 PM Report Abusive Post Report Copyright Violation | |
Mr. Chimpington
User ID: 84704393 United States 11/27/2022 06:02 PM Report Abusive Post Report Copyright Violation | |
BrainGuy, MAGA Republican
White heteropatriarchal supremacist chemophob User ID: 84804751 United States 11/27/2022 06:21 PM Report Abusive Post Report Copyright Violation | |
Dijact
User ID: 84453882 United States 11/27/2022 06:27 PM Report Abusive Post Report Copyright Violation | |
JustSomeGuy_42
User ID: 84491289 United States 11/27/2022 07:14 PM Report Abusive Post Report Copyright Violation | Man, there is no fucking way a grown ass man thought the rocket was going straight to the moon. Quoting: Dijact Yes, way. And I'll bet some of 'em have Liberal Arts degrees. Warning: JustSomeGuy_42 is a publicly confessed unvaxxed neophiliac . If the number 666 is considered evil. then technically, 25.8069758 is the root of all evil. |
Fugazi World
User ID: 74550637 United States 11/27/2022 07:36 PM Report Abusive Post Report Copyright Violation | But, but, 53 years ago they landed on the moon effortlessly. It was as easy as putting your foot in a shoe. Now here we are 5 decades later with technology advanced about 50 thousand times yet they misses the moon??? I dunno. Maybe it’s just me but that sounds a tad, how you say?? Fishy. Last Edited by Fugazi World on 11/27/2022 07:37 PM Fugazi World |
Deplorableduckhunter
User ID: 83942891 United States 11/27/2022 07:42 PM Report Abusive Post Report Copyright Violation | |
Astromut
(OP) Senior Forum Moderator 11/28/2022 07:49 AM Report Abusive Post Report Copyright Violation | |
scimitar
User ID: 77713000 United States 11/28/2022 05:57 PM Report Abusive Post Report Copyright Violation | IDW is still around here, he just doesn't use his screen name because he knows he's ban on sight. He likes to make threats and such to this day. Quoting: Astromut Anyway, to get to the meat of your question, yes the trajectory here is very different. SLS is a very different animal than the Saturn V, though both are super heavy lift. Saturn V had three stages, SLS has two solid boosters, a large core stage and at the moment a small "interim" upper stage. The Orion's service module does not have as much fuel and delta-V as the Apollo CSM had. To give you an idea, the Apollo CSM carried about 18,410 kg of propellant for the main SPS engine and the Apollo command module was a smaller capsule than Orion. Orion's European Service Module only has a propellant mass of about 8,600 kg and carries a heavier capsule. Ironically, both the CSM and European Service Module rely on versions of the AJ-10 engine, though Orion's is literally an old Space Shuttle OMS engine that has been repurposed for one more flight. Orion with its current service module cannot perform the mission profiles that Apollo's CSM could. It can't carry a lander into low lunar orbit and then get itself out of low lunar orbit for a return to earth. Likewise, the ICPS is very under-powered compared to the mighty Saturn V upper stage, the S-IVB. The ICPS is really just a modified Delta upper stage, and it only carries about 28,576 kg of propellant mass vs 109,000 kg for the S-IVB. The upgraded Exploration Upper Stage or EUS will flip that statistic later on, but for now the ICPS is what Orion had to work with. Given these limitations and the nature of the SLS rocket's staging, the core stage put Orion and the ICPS into a slightly elliptical parking orbit that essentially gave the ICPS a "head-start" before the TLI burn (on the Saturn V, the S-IVB finished the orbit insertion itself and stayed in a low parking orbit until TLI). Even so, the ICPS and Orion cannot fly the kind of profile we saw with Apollo, so they opted for an easier but slower trajectory to a distant retrograde orbit of the moon, swinging wide past the moon each time and never braking fully into a low lunar orbit. This is similar to how later missions will utilize a halo orbit that stays farther from the moon than Apollo and a lunar lander that will meet Orion there and depart to the surface from a wider starting orbit. This trajectory does not require as much delta-V from Orion to do the mission and still get back to earth. Thank you for that incredibly detailed explanation. Sorry I took so long to respond, but even though I'm retired there is always a distraction.... I have too many things to tend to. I realize some might say change things to simplify my life, but it just wouldn't be me. Take care, I wish for you a great holiday season. Ominous regressions One Truth... many realities |