Author Topic: SpaceX Falcon Heavy Discussion (Thread 6)  (Read 551560 times)

Offline Jim

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Re: SpaceX Falcon Heavy Discussion (Thread 6)
« Reply #440 on: 02/04/2018 11:50 am »
Or can we do better, something we can use to convince the misguided scientist putting his faith in government statisticians?

Who and what government statisticians?

Re: SpaceX Falcon Heavy Discussion (Thread 6)
« Reply #441 on: 02/04/2018 12:10 pm »
I don't think Doug Ellison is capable of talking about anything SpaceX related objectively. He's quick to pull the trigger whenever he finds the opportunity to criticize SpaceX, sometime sacrificing in-depth research of what he's saying when something confirms his already negative opinion of the company.
That's especially true when talking about Falcon performance figures: I remember him trying to pass the narrative that SpaceX has greatly increased the price of Falcon 9, failing to account for inflation and for the fact that, even with recovery, today's Falcon 9 has a payload capacity greater than 2010 F9 expendable. I politely told him and his answer was to quickly block me on Twitter.
Also if something is unclear and he has to make an estimate, he always assumes the worst for SpaceX, never giving them the benefit of the doubt. 
Definitely not a reasonable guy when it comes to SpaceX.
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Offline Hominans Kosmos

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Re: SpaceX Falcon Heavy Discussion (Thread 6)
« Reply #442 on: 02/04/2018 01:12 pm »
Or can we do better, something we can use to convince the misguided scientist putting his faith in government statisticians?

Who and what government statisticians?

You're right. I've misspoken, no statisticians on staff https://elvperf.ksc.nasa.gov/Pages/Contacts.aspx

Offline Svetoslav

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Re: SpaceX Falcon Heavy Discussion (Thread 6)
« Reply #443 on: 02/04/2018 01:25 pm »
I don't think Doug Ellison is capable of talking about anything SpaceX related objectively. He's quick to pull the trigger whenever he finds the opportunity to criticize SpaceX, sometime sacrificing in-depth research of what he's saying when something confirms his already negative opinion of the company.
That's especially true when talking about Falcon performance figures: I remember him trying to pass the narrative that SpaceX has greatly increased the price of Falcon 9, failing to account for inflation and for the fact that, even with recovery, today's Falcon 9 has a payload capacity greater than 2010 F9 expendable. I politely told him and his answer was to quickly block me on Twitter.
Also if something is unclear and he has to make an estimate, he always assumes the worst for SpaceX, never giving them the benefit of the doubt. 
Definitely not a reasonable guy when it comes to SpaceX.

I'm also blocked by Doug Ellison, and thus, forever banned from UMSF. Can someone point out what this tweet is about, as I'm not worthy enough to read it?
« Last Edit: 02/04/2018 01:26 pm by Svetoslav »

Offline Lar

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Re: SpaceX Falcon Heavy Discussion (Thread 6)
« Reply #444 on: 02/04/2018 01:36 pm »
UMSF?
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Offline Svetoslav

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Re: SpaceX Falcon Heavy Discussion (Thread 6)
« Reply #445 on: 02/04/2018 01:40 pm »
UMSF?

Unmanned spaceflight forum. Sorry, didn't have to bring personal issues on this board. Still... can anyone say what the discussion on Twitter is about, as some of us can't read it?

Offline JoerTex

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Re: SpaceX Falcon Heavy Discussion (Thread 6)
« Reply #446 on: 02/04/2018 02:02 pm »
Please use private communication for the reply.

This is a SpaceX forum.

Offline Svetoslav

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Re: SpaceX Falcon Heavy Discussion (Thread 6)
« Reply #447 on: 02/04/2018 02:06 pm »
Never mind, I found a way to read the discussion.

Do I get it right? Falcon Heavy doesn't have an efficient upper stage and that's why the rocket is inferior to other expendable rockets when it comes to interplanetary missions?

Offline octavo

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Re: SpaceX Falcon Heavy Discussion (Thread 6)
« Reply #448 on: 02/04/2018 02:15 pm »
Never mind, I found a way to read the discussion.

Do I get it right? Falcon Heavy doesn't have an efficient upper stage and that's why the rocket is inferior to other expendable rockets when it comes to interplanetary missions?
Yep.

Offline guckyfan

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Re: SpaceX Falcon Heavy Discussion (Thread 6)
« Reply #449 on: 02/04/2018 02:24 pm »
Never mind, I found a way to read the discussion.

Do I get it right? Falcon Heavy doesn't have an efficient upper stage and that's why the rocket is inferior to other expendable rockets when it comes to interplanetary missions?
Yep.

But that disadvantage makes FH inferior to Delta 4 Heavy only beyond Mars. Plus it can be at least partly remedied by giving the payload an additional kickstage, taking advantage of the higher payload capacity to lower energetic trajectories. Despite the upper stage FH is still an incredibly powerful launch vehicle even for high energy trajectories.

Offline Svetoslav

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Re: SpaceX Falcon Heavy Discussion (Thread 6)
« Reply #450 on: 02/04/2018 02:28 pm »
That's exactly what I wanted to ask. If Falcon Heavy is all about putting 60ish tons in LEO, what would prevent adding a cryo upper stage?

Offline Hominans Kosmos

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Re: SpaceX Falcon Heavy Discussion (Thread 6)
« Reply #451 on: 02/04/2018 02:28 pm »
Never mind, I found a way to read the discussion.

Do I get it right? Falcon Heavy doesn't have an efficient upper stage and that's why the rocket is inferior to other expendable rockets when it comes to interplanetary missions?
Yep.

But that disadvantage makes FH inferior to Delta 4 Heavy only beyond Mars. Plus it can be at least partly remedied by giving the payload an additional kickstage, taking advantage of the higher payload capacity to lower energetic trajectories. Despite the upper stage FH is still an incredibly powerful launch vehicle even for high energy trajectories.

I'm finding my limited mathematical and programming qualifications make getting that point across over at the FB group difficult.

Online Robotbeat

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Re: SpaceX Falcon Heavy Discussion (Thread 6)
« Reply #452 on: 02/04/2018 02:44 pm »
Never mind, I found a way to read the discussion.

Do I get it right? Falcon Heavy doesn't have an efficient upper stage and that's why the rocket is inferior to other expendable rockets when it comes to interplanetary missions?
Yep.

But that disadvantage makes FH inferior to Delta 4 Heavy only beyond Mars. Plus it can be at least partly remedied by giving the payload an additional kickstage, taking advantage of the higher payload capacity to lower energetic trajectories. Despite the upper stage FH is still an incredibly powerful launch vehicle even for high energy trajectories.
Not even /partially/ mitigated: ENTIRELY mitigated.

Doug was being disingenuous. You would not launch a large payload to such high energy trajectories on any EELV or Falcon without a kick stage. Atlas V with kick stage is cheaper & higher performance than D4H without one (which is partly why New Horizons did just that), and FH plus kick stage beats them both.
« Last Edit: 02/04/2018 02:49 pm by Robotbeat »
Chris  Whoever loves correction loves knowledge, but he who hates reproof is stupid.

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Online Robotbeat

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Re: SpaceX Falcon Heavy Discussion (Thread 6)
« Reply #453 on: 02/04/2018 02:51 pm »
That's exactly what I wanted to ask. If Falcon Heavy is all about putting 60ish tons in LEO, what would prevent adding a cryo upper stage?
Simply stretching the upper stage of FH would basically null out any performance difference. And adding a kick stage on top of *that* would allow FH to launch Europa Clipper direct to Jupiter like SLS.
Chris  Whoever loves correction loves knowledge, but he who hates reproof is stupid.

To the maximum extent practicable, the Federal Government shall plan missions to accommodate the space transportation services capabilities of United States commercial providers. US law http://goo.gl/YZYNt0

Offline Ictogan

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Re: SpaceX Falcon Heavy Discussion (Thread 6)
« Reply #454 on: 02/04/2018 02:52 pm »
That's exactly what I wanted to ask. If Falcon Heavy is all about putting 60ish tons in LEO, what would prevent adding a cryo upper stage?
1. Development costs
2. extreme fineness ratio of the vehicle+GSE incompability if the cryogenic stage would be part of the vehicle stack
3. taking up a large portion of the fairing volume and having to figure out how to fuel it in the fairings if it would be in the fairings

Offline Jim

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Re: SpaceX Falcon Heavy Discussion (Thread 6)
« Reply #455 on: 02/04/2018 02:53 pm »
Doug was being disingenuous. You would not launch a large payload to such high energy trajectories on any EELV or Falcon without a kick stage. Atlas V with kick stage is cheaper & higher performance than D4H without one (which is partly why New Horizons did just that), and FH plus kick stage beats them both.

Not true.  Only high speed missions like PNH and PSP need kick stages. Mars, Jupiter and Saturn missions don't and that is where FH falls short.

Offline dglow

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Re: SpaceX Falcon Heavy Discussion (Thread 6)
« Reply #456 on: 02/04/2018 02:58 pm »
3. taking up a large portion of the fairing volume and having to figure out how to fuel it in the fairings if it would be in the fairings

I've always wondered about this. (slightly OT, apologies) What is the reason for Atlas V's fairing encapsulating (much of) Centaur?

Offline Jim

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Re: SpaceX Falcon Heavy Discussion (Thread 6)
« Reply #457 on: 02/04/2018 02:58 pm »
Simply stretching the upper stage of FH would basically null out any performance difference. And adding a kick stage on top of *that* would allow FH to launch Europa Clipper direct to Jupiter like SLS.

There is no kick stage for Europa Clipper on FH.  "Kick" stages are solid motors which have high thrust.  Solid motors and Falcon are none starters.

There is no stretching of the upperstage.  there is no more F9 development.

Europa Clipper on FH would use gravity assists.

Offline Jim

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Re: SpaceX Falcon Heavy Discussion (Thread 6)
« Reply #458 on: 02/04/2018 02:58 pm »
3. taking up a large portion of the fairing volume and having to figure out how to fuel it in the fairings if it would be in the fairings

I've always wondered about this. (slightly OT, apologies) What is the reason for Atlas V's fairing encapsulating (much of) Centaur?

Aeroloads with the big fairing

Online Robotbeat

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Re: SpaceX Falcon Heavy Discussion (Thread 6)
« Reply #459 on: 02/04/2018 03:00 pm »
Doug was being disingenuous. You would not launch a large payload to such high energy trajectories on any EELV or Falcon without a kick stage. Atlas V with kick stage is cheaper & higher performance than D4H without one (which is partly why New Horizons did just that), and FH plus kick stage beats them both.

Not true.  Only high speed missions like PNH and PSP need kick stages. Mars, Jupiter and Saturn missions don't and that is where FH falls short.
He was looking basically exclusively at high energy missions, higher energy than the typical deep space missions which use multiple gravity assists.

To Mars, FH also beats Atlas V handily.
Chris  Whoever loves correction loves knowledge, but he who hates reproof is stupid.

To the maximum extent practicable, the Federal Government shall plan missions to accommodate the space transportation services capabilities of United States commercial providers. US law http://goo.gl/YZYNt0

 

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