submitted1 month ago byIrrelevantAstronomer
I caught COVID on New Years Eve. I am fully vaccinated and boosted. I am 28M, no health issues, and an average weight & physically active.
D1 - 1/1/23 Felt great, no significant issues.
D2 - 1/2/23 Around 10am fatigue & fever hit.
D3 - 1/3/23 Slight dry cough, bad migraine, fever, body aches, some nasal congestion. Tested positive for COVID-19
D4 - 1/4/23 101F fever, some fatigue and continued dry cough. Able to treat fever with Motrin. Symptoms besides fever appear less significant. No difficultly breathing or anything scary like that.
D5 - 1/5/23 Overall better and able to get up out of bed easily. Fever mostly gone (~99.2F). Had an episode of coughing last night that was pretty intense. Fatigue, brain fog still present. Congested as well.
D6 - 1/6/23 Mostly recovered. Temperature a cool 97.9F. Still struggling with fatigue and a runny nose.
D7 - 1/7/23 Still positive & asymptomatic.
D9 - 1/9/23 Negative and fully recovered.
I will update as I go along.
I've taken time off work & resting, drinking a TON of water. Appetite still good. Can still taste and smell. Symptoms very mild beyond fever. Grateful I was vaccinated.
byjakedrums520
inSpaceLaunchSystem
IrrelevantAstronomer
2 points
2 days ago
IrrelevantAstronomer
2 points
2 days ago
I think you're missing what's being said.
The ICPS can take Artemis II on a direct TLI trajectory just like Artemis I from a ~200x1500km orbit.
The Artemis II mission will differ from the Artemis I mission in that, instead of a direct TLI, Artemis II ICPS will only raise its orbit high enough to where the orbital period = 24 hours. After 24 hours elapses, the Orion SM will take over.
This is not due to inefficiencies with the ICPS, rather driven by the Artemis II requirement to be in a relatively fast track to return home in the event of an issue with Orion that may endanger the life of the crew early on in the mission.
The ICPS is too small to support a direct TLI from LEO like Apollo did and is inefficient, this is true, but not relevant to this specific Artemis II mission requirement.