Author Topic: Starship Expendable Upper Stage?  (Read 83122 times)

Offline Paul451

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Re: Starship Expendable Upper Stage?
« Reply #160 on: 01/30/2025 09:22 pm »
While Enceladus has significant atmosphere

Not "significant" in the sense that you mean; statistically significant, detectably above the pressure that would naturally occur without geysers. In the sense that the Earth's moon had an "atmosphere" during the Apollo program.

"Trace gases" by any other standard.

Paul451 just sent me a PM with a very germane fact:

But not germane to the topic.

Offline TomH

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Re: Starship Expendable Upper Stage?
« Reply #161 on: 01/30/2025 09:49 pm »
I agree that the thread topic has drifted. Yet it a discussion worth having, so I have created a new thread to continue the discussion:

https://forum.nasaspaceflight.com/index.php?topic=62325.0

Offline aporigine

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Re: Expendable Upper Stage?!?
« Reply #162 on: 02/01/2025 02:43 pm »


(edit) removed reply to a two-year-old post. Percussive processing of deceased equine.
« Last Edit: 02/01/2025 02:46 pm by aporigine »

Offline Twark_Main

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Re: Starship Expendable Upper Stage?
« Reply #163 on: 02/01/2025 04:37 pm »
Expendable would be best utilized for an unusually large deep space probe, which would be a rare mission. Enceladus and Europa have oceans with a frozen surface. A mission might have:

1) A lander
2) A stationary communications relay that stays with the lander
3) A nuclear powered mini submarine which melts its way through the ice, unspools a communication
    cable as it does so, then leaves a signal relay station at the bottom of the ice. The sub then goes
    off to explore the submerged world.

Again, this would be rare and it would be high mass. If done in an architecture with non-distributed mass, a disposable US makes sense. A fairing is jettisoned upon reaching vacuum, and the US is re-propped in LEO, possibly again in cis-lunar space. The second stage in essence is reused as both a third stage, and possibly even a fourth stage, simply by taking on additional prop at specified waypoints.

Why would you jettison a fairing?  You waste up to 10km/sec of aerocapture potential

You eliminate all atmospheric paraphernalia on the US: tiles, elonerons, and jettison the fairing. The lander itself has its own much smaller TPS and landing system. This is advantageous in mass trades. Rather than managing the mass of an entire Starship entering the atmosphere of Enceladus, you have something similar to (but larger than) a Curiosity/Perseverance EDL architecture.


And here I thought IE was referring to keeping just the fairing. Lots of potential braking surface area but much lower mass.

 

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