Break Away Valves for Launch The Next CEO of Stack OverflowWhat rocket uses the largest percentage of Fuel/Oxidizer before liftoff?Could escape velocity be achieved in the atmosphere?How much fuel would one need to launch a 1kg object from 100,000 feet?How much fuel was used for a Space Shuttle launch?What is a typical energy demand and carbon footprint of a space launch?How do they get up-close views of far away spacecraft after launch?How far away can one see a NASA rocket launch?Good source for launch videosIs the pressurization of propellant tanks necessary for structural integrity?Odor of a rocket launch?Why rockets are not tossed up before launchReaction Drive Launch Catapult
Beveled cylinder cutout
Is it possible to replace duplicates of a character with one character using tr
Would this house-rule that treats advantage as a +1 to the roll instead (and disadvantage as -1) and allows them to stack be balanced?
Won the lottery - how do I keep the money?
What does "Its cash flow is deeply negative" mean?
Why is my new battery behaving weirdly?
Is wanting to ask what to write an indication that you need to change your story?
What was the first Unix version to run on a microcomputer?
Chain wire methods together in Lightning Web Components
Why doesn't UK go for the same deal Japan has with EU to resolve Brexit?
unclear about Dynamic Binding
Is it my responsibility to learn a new technology in my own time my employer wants to implement?
Example of a Mathematician/Physicist whose Other Publications during their PhD eclipsed their PhD Thesis
How did people program for Consoles with multiple CPUs?
Why isn't the Mueller report being released completely and unredacted?
Newlines in BSD sed vs gsed
How do I align (1) and (2)?
Recycling old answers
Reference request: Grassmannian and Plucker coordinates in type B, C, D
Why, when going from special to general relativity, do we just replace partial derivatives with covariant derivatives?
Help understanding this unsettling image of Titan, Epimetheus, and Saturn's rings?
Plot of histogram similar to output from @risk
Solving system of ODEs with extra parameter
What steps are necessary to read a Modern SSD in Medieval Europe?
Break Away Valves for Launch
The Next CEO of Stack OverflowWhat rocket uses the largest percentage of Fuel/Oxidizer before liftoff?Could escape velocity be achieved in the atmosphere?How much fuel would one need to launch a 1kg object from 100,000 feet?How much fuel was used for a Space Shuttle launch?What is a typical energy demand and carbon footprint of a space launch?How do they get up-close views of far away spacecraft after launch?How far away can one see a NASA rocket launch?Good source for launch videosIs the pressurization of propellant tanks necessary for structural integrity?Odor of a rocket launch?Why rockets are not tossed up before launchReaction Drive Launch Catapult
$begingroup$
I forgot to hang up the fuel pump and broke it off and costed around 80 dollars to replace. While there I wandered could this be adapted to a rocket in some way?
How much fuel capacity would be saved if the fuel was fed to the rocket to keep it topped off until it has fully left the launch tower? The length of the fuel line and break away valve would be the height of the launch tower.
Could it be fed through an extended tower with a fuel line that travels aside the rocket not to burden the rocket with the weight of the fuel line or cause a whip in the fuel line?

https://sputniknews.com/science/201812291071085215-soyuz-launch-russia-uk-satellite/
launch fuel engines design-alternative
$endgroup$
add a comment |
$begingroup$
I forgot to hang up the fuel pump and broke it off and costed around 80 dollars to replace. While there I wandered could this be adapted to a rocket in some way?
How much fuel capacity would be saved if the fuel was fed to the rocket to keep it topped off until it has fully left the launch tower? The length of the fuel line and break away valve would be the height of the launch tower.
Could it be fed through an extended tower with a fuel line that travels aside the rocket not to burden the rocket with the weight of the fuel line or cause a whip in the fuel line?

https://sputniknews.com/science/201812291071085215-soyuz-launch-russia-uk-satellite/
launch fuel engines design-alternative
$endgroup$
add a comment |
$begingroup$
I forgot to hang up the fuel pump and broke it off and costed around 80 dollars to replace. While there I wandered could this be adapted to a rocket in some way?
How much fuel capacity would be saved if the fuel was fed to the rocket to keep it topped off until it has fully left the launch tower? The length of the fuel line and break away valve would be the height of the launch tower.
Could it be fed through an extended tower with a fuel line that travels aside the rocket not to burden the rocket with the weight of the fuel line or cause a whip in the fuel line?

https://sputniknews.com/science/201812291071085215-soyuz-launch-russia-uk-satellite/
launch fuel engines design-alternative
$endgroup$
I forgot to hang up the fuel pump and broke it off and costed around 80 dollars to replace. While there I wandered could this be adapted to a rocket in some way?
How much fuel capacity would be saved if the fuel was fed to the rocket to keep it topped off until it has fully left the launch tower? The length of the fuel line and break away valve would be the height of the launch tower.
Could it be fed through an extended tower with a fuel line that travels aside the rocket not to burden the rocket with the weight of the fuel line or cause a whip in the fuel line?

https://sputniknews.com/science/201812291071085215-soyuz-launch-russia-uk-satellite/
launch fuel engines design-alternative
launch fuel engines design-alternative
edited 1 hour ago
Muze
asked 2 hours ago
MuzeMuze
1,3241264
1,3241264
add a comment |
add a comment |
1 Answer
1
active
oldest
votes
$begingroup$
Theoretically yes. However there are concerns:
1) Propellant load is dangerous under the best circumstances. Add in all the vibration loads of an "on" rocket and you have a doozie.
2) Most rockets already have umbilicals that disconnect slightly after liftoff. The recent Rocketlab launch video has a good angle of this
3) It's a bit of added weight and complexity.
These are all surmountable, but then what would you be gaining? I'm sure someone can do a calculation (slightly related to this question) but I suspect it's a negligible amount of payload/mass gain.
$endgroup$
$begingroup$
If you think about it it is saved weight need less fuel storage.
$endgroup$
– Muze
52 mins ago
$begingroup$
Could you clarify?
$endgroup$
– randomUsername
49 mins ago
$begingroup$
You can off set the onboard fuel needed for the mission saving weight for heavier payload.
$endgroup$
– Muze
43 mins ago
add a comment |
Your Answer
StackExchange.ifUsing("editor", function ()
return StackExchange.using("mathjaxEditing", function ()
StackExchange.MarkdownEditor.creationCallbacks.add(function (editor, postfix)
StackExchange.mathjaxEditing.prepareWmdForMathJax(editor, postfix, [["$", "$"], ["\\(","\\)"]]);
);
);
, "mathjax-editing");
StackExchange.ready(function()
var channelOptions =
tags: "".split(" "),
id: "508"
;
initTagRenderer("".split(" "), "".split(" "), channelOptions);
StackExchange.using("externalEditor", function()
// Have to fire editor after snippets, if snippets enabled
if (StackExchange.settings.snippets.snippetsEnabled)
StackExchange.using("snippets", function()
createEditor();
);
else
createEditor();
);
function createEditor()
StackExchange.prepareEditor(
heartbeatType: 'answer',
autoActivateHeartbeat: false,
convertImagesToLinks: false,
noModals: true,
showLowRepImageUploadWarning: true,
reputationToPostImages: null,
bindNavPrevention: true,
postfix: "",
imageUploader:
brandingHtml: "Powered by u003ca class="icon-imgur-white" href="https://imgur.com/"u003eu003c/au003e",
contentPolicyHtml: "User contributions licensed under u003ca href="https://creativecommons.org/licenses/by-sa/3.0/"u003ecc by-sa 3.0 with attribution requiredu003c/au003e u003ca href="https://stackoverflow.com/legal/content-policy"u003e(content policy)u003c/au003e",
allowUrls: true
,
noCode: true, onDemand: true,
discardSelector: ".discard-answer"
,immediatelyShowMarkdownHelp:true
);
);
Sign up or log in
StackExchange.ready(function ()
StackExchange.helpers.onClickDraftSave('#login-link');
);
Sign up using Google
Sign up using Facebook
Sign up using Email and Password
Post as a guest
Required, but never shown
StackExchange.ready(
function ()
StackExchange.openid.initPostLogin('.new-post-login', 'https%3a%2f%2fspace.stackexchange.com%2fquestions%2f35169%2fbreak-away-valves-for-launch%23new-answer', 'question_page');
);
Post as a guest
Required, but never shown
1 Answer
1
active
oldest
votes
1 Answer
1
active
oldest
votes
active
oldest
votes
active
oldest
votes
$begingroup$
Theoretically yes. However there are concerns:
1) Propellant load is dangerous under the best circumstances. Add in all the vibration loads of an "on" rocket and you have a doozie.
2) Most rockets already have umbilicals that disconnect slightly after liftoff. The recent Rocketlab launch video has a good angle of this
3) It's a bit of added weight and complexity.
These are all surmountable, but then what would you be gaining? I'm sure someone can do a calculation (slightly related to this question) but I suspect it's a negligible amount of payload/mass gain.
$endgroup$
$begingroup$
If you think about it it is saved weight need less fuel storage.
$endgroup$
– Muze
52 mins ago
$begingroup$
Could you clarify?
$endgroup$
– randomUsername
49 mins ago
$begingroup$
You can off set the onboard fuel needed for the mission saving weight for heavier payload.
$endgroup$
– Muze
43 mins ago
add a comment |
$begingroup$
Theoretically yes. However there are concerns:
1) Propellant load is dangerous under the best circumstances. Add in all the vibration loads of an "on" rocket and you have a doozie.
2) Most rockets already have umbilicals that disconnect slightly after liftoff. The recent Rocketlab launch video has a good angle of this
3) It's a bit of added weight and complexity.
These are all surmountable, but then what would you be gaining? I'm sure someone can do a calculation (slightly related to this question) but I suspect it's a negligible amount of payload/mass gain.
$endgroup$
$begingroup$
If you think about it it is saved weight need less fuel storage.
$endgroup$
– Muze
52 mins ago
$begingroup$
Could you clarify?
$endgroup$
– randomUsername
49 mins ago
$begingroup$
You can off set the onboard fuel needed for the mission saving weight for heavier payload.
$endgroup$
– Muze
43 mins ago
add a comment |
$begingroup$
Theoretically yes. However there are concerns:
1) Propellant load is dangerous under the best circumstances. Add in all the vibration loads of an "on" rocket and you have a doozie.
2) Most rockets already have umbilicals that disconnect slightly after liftoff. The recent Rocketlab launch video has a good angle of this
3) It's a bit of added weight and complexity.
These are all surmountable, but then what would you be gaining? I'm sure someone can do a calculation (slightly related to this question) but I suspect it's a negligible amount of payload/mass gain.
$endgroup$
Theoretically yes. However there are concerns:
1) Propellant load is dangerous under the best circumstances. Add in all the vibration loads of an "on" rocket and you have a doozie.
2) Most rockets already have umbilicals that disconnect slightly after liftoff. The recent Rocketlab launch video has a good angle of this
3) It's a bit of added weight and complexity.
These are all surmountable, but then what would you be gaining? I'm sure someone can do a calculation (slightly related to this question) but I suspect it's a negligible amount of payload/mass gain.
answered 55 mins ago
randomUsernamerandomUsername
33118
33118
$begingroup$
If you think about it it is saved weight need less fuel storage.
$endgroup$
– Muze
52 mins ago
$begingroup$
Could you clarify?
$endgroup$
– randomUsername
49 mins ago
$begingroup$
You can off set the onboard fuel needed for the mission saving weight for heavier payload.
$endgroup$
– Muze
43 mins ago
add a comment |
$begingroup$
If you think about it it is saved weight need less fuel storage.
$endgroup$
– Muze
52 mins ago
$begingroup$
Could you clarify?
$endgroup$
– randomUsername
49 mins ago
$begingroup$
You can off set the onboard fuel needed for the mission saving weight for heavier payload.
$endgroup$
– Muze
43 mins ago
$begingroup$
If you think about it it is saved weight need less fuel storage.
$endgroup$
– Muze
52 mins ago
$begingroup$
If you think about it it is saved weight need less fuel storage.
$endgroup$
– Muze
52 mins ago
$begingroup$
Could you clarify?
$endgroup$
– randomUsername
49 mins ago
$begingroup$
Could you clarify?
$endgroup$
– randomUsername
49 mins ago
$begingroup$
You can off set the onboard fuel needed for the mission saving weight for heavier payload.
$endgroup$
– Muze
43 mins ago
$begingroup$
You can off set the onboard fuel needed for the mission saving weight for heavier payload.
$endgroup$
– Muze
43 mins ago
add a comment |
Thanks for contributing an answer to Space Exploration Stack Exchange!
- Please be sure to answer the question. Provide details and share your research!
But avoid …
- Asking for help, clarification, or responding to other answers.
- Making statements based on opinion; back them up with references or personal experience.
Use MathJax to format equations. MathJax reference.
To learn more, see our tips on writing great answers.
Sign up or log in
StackExchange.ready(function ()
StackExchange.helpers.onClickDraftSave('#login-link');
);
Sign up using Google
Sign up using Facebook
Sign up using Email and Password
Post as a guest
Required, but never shown
StackExchange.ready(
function ()
StackExchange.openid.initPostLogin('.new-post-login', 'https%3a%2f%2fspace.stackexchange.com%2fquestions%2f35169%2fbreak-away-valves-for-launch%23new-answer', 'question_page');
);
Post as a guest
Required, but never shown
Sign up or log in
StackExchange.ready(function ()
StackExchange.helpers.onClickDraftSave('#login-link');
);
Sign up using Google
Sign up using Facebook
Sign up using Email and Password
Post as a guest
Required, but never shown
Sign up or log in
StackExchange.ready(function ()
StackExchange.helpers.onClickDraftSave('#login-link');
);
Sign up using Google
Sign up using Facebook
Sign up using Email and Password
Post as a guest
Required, but never shown
Sign up or log in
StackExchange.ready(function ()
StackExchange.helpers.onClickDraftSave('#login-link');
);
Sign up using Google
Sign up using Facebook
Sign up using Email and Password
Sign up using Google
Sign up using Facebook
Sign up using Email and Password
Post as a guest
Required, but never shown
Required, but never shown
Required, but never shown
Required, but never shown
Required, but never shown
Required, but never shown
Required, but never shown
Required, but never shown
Required, but never shown