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NASA's RS-25 Engines
What should a Discovery Program mission budget look like?What are the costs of the various different engines in current use?How did they solve Saturn V pogo oscillation problems?Nasa's Orion program doesn't make senseHow will the SLS first stage be supplied with engines? Copy manufacturing the RS-25 or replacing it?Are cold gas thrusters viable for model rockets?How is chamber pressure and temperature determined for cold gas thrusters?What does this paper say is wrong (quantitatively and procedurally) with WISE & NeoWISE asteroid data?Where can I read further on the specs the South Korean engine for next month's sub-orbital test?How will the Gateway-before-boots sequence benefit US business, economic and technological development?
$begingroup$
I am developing a FSX-based space flight simulator FSX SpacePort. I've been trying to get the detailed specs on NASA's RS-25 engine, namely, what were the ramp-up times for this engine? As in, how long did it take from ignition to full thrust?
Thanks!
nasa engines sls ssme
New contributor
$endgroup$
add a comment |
$begingroup$
I am developing a FSX-based space flight simulator FSX SpacePort. I've been trying to get the detailed specs on NASA's RS-25 engine, namely, what were the ramp-up times for this engine? As in, how long did it take from ignition to full thrust?
Thanks!
nasa engines sls ssme
New contributor
$endgroup$
add a comment |
$begingroup$
I am developing a FSX-based space flight simulator FSX SpacePort. I've been trying to get the detailed specs on NASA's RS-25 engine, namely, what were the ramp-up times for this engine? As in, how long did it take from ignition to full thrust?
Thanks!
nasa engines sls ssme
New contributor
$endgroup$
I am developing a FSX-based space flight simulator FSX SpacePort. I've been trying to get the detailed specs on NASA's RS-25 engine, namely, what were the ramp-up times for this engine? As in, how long did it take from ignition to full thrust?
Thanks!
nasa engines sls ssme
nasa engines sls ssme
New contributor
New contributor
edited 3 hours ago
Organic Marble
58.2k3159249
58.2k3159249
New contributor
asked 5 hours ago
Mitch99Mitch99
254
254
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New contributor
add a comment |
add a comment |
1 Answer
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A good assumption is that the startup sequence is very similar to the SSME. Here is some SSME startup data showing the time you asked about from the Rocketdyne Pocket Data Book. Eventually the SLS will be using RS-25Es which are somewhat different from the SSME, but my guess is that the start sequence won't change much if at all.
The hashed field is test experience, the solid lines are the ICD requirements.
$endgroup$
$begingroup$
Awesome! Exactly what I was looking for! Thank you!
$endgroup$
– Mitch99
2 hours ago
$begingroup$
@Mitch99 Since you're new to the site: If this answer is what you were looking for, please mark it as correct by clicking the gray checkmark beside it. And upvote if you have a mind to.
$endgroup$
– Organic Marble
2 hours ago
$begingroup$
Got it, thanks!!
$endgroup$
– Mitch99
1 hour ago
$begingroup$
So - since it takes ~4 seconds to get them to 100% thrust, do they then ignite them at T -4:00 seconds, and they count T -0:00 the time all of them are roughly at 100%, the SRBs get lit, and it's a "mission start"?
$endgroup$
– Mitch99
1 hour ago
$begingroup$
I only know about shuttle, but there the start command was send at ~T-5 seconds, which gave time for the SSMEs to light, the "twang" to settle, and then the SRBs lit at, yes, T-0. SLS won't have the "twang" to deal with because its engines are axially mounted.
$endgroup$
– Organic Marble
1 hour ago
|
show 2 more comments
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1 Answer
1
active
oldest
votes
1 Answer
1
active
oldest
votes
active
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votes
active
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votes
$begingroup$
A good assumption is that the startup sequence is very similar to the SSME. Here is some SSME startup data showing the time you asked about from the Rocketdyne Pocket Data Book. Eventually the SLS will be using RS-25Es which are somewhat different from the SSME, but my guess is that the start sequence won't change much if at all.
The hashed field is test experience, the solid lines are the ICD requirements.
$endgroup$
$begingroup$
Awesome! Exactly what I was looking for! Thank you!
$endgroup$
– Mitch99
2 hours ago
$begingroup$
@Mitch99 Since you're new to the site: If this answer is what you were looking for, please mark it as correct by clicking the gray checkmark beside it. And upvote if you have a mind to.
$endgroup$
– Organic Marble
2 hours ago
$begingroup$
Got it, thanks!!
$endgroup$
– Mitch99
1 hour ago
$begingroup$
So - since it takes ~4 seconds to get them to 100% thrust, do they then ignite them at T -4:00 seconds, and they count T -0:00 the time all of them are roughly at 100%, the SRBs get lit, and it's a "mission start"?
$endgroup$
– Mitch99
1 hour ago
$begingroup$
I only know about shuttle, but there the start command was send at ~T-5 seconds, which gave time for the SSMEs to light, the "twang" to settle, and then the SRBs lit at, yes, T-0. SLS won't have the "twang" to deal with because its engines are axially mounted.
$endgroup$
– Organic Marble
1 hour ago
|
show 2 more comments
$begingroup$
A good assumption is that the startup sequence is very similar to the SSME. Here is some SSME startup data showing the time you asked about from the Rocketdyne Pocket Data Book. Eventually the SLS will be using RS-25Es which are somewhat different from the SSME, but my guess is that the start sequence won't change much if at all.
The hashed field is test experience, the solid lines are the ICD requirements.
$endgroup$
$begingroup$
Awesome! Exactly what I was looking for! Thank you!
$endgroup$
– Mitch99
2 hours ago
$begingroup$
@Mitch99 Since you're new to the site: If this answer is what you were looking for, please mark it as correct by clicking the gray checkmark beside it. And upvote if you have a mind to.
$endgroup$
– Organic Marble
2 hours ago
$begingroup$
Got it, thanks!!
$endgroup$
– Mitch99
1 hour ago
$begingroup$
So - since it takes ~4 seconds to get them to 100% thrust, do they then ignite them at T -4:00 seconds, and they count T -0:00 the time all of them are roughly at 100%, the SRBs get lit, and it's a "mission start"?
$endgroup$
– Mitch99
1 hour ago
$begingroup$
I only know about shuttle, but there the start command was send at ~T-5 seconds, which gave time for the SSMEs to light, the "twang" to settle, and then the SRBs lit at, yes, T-0. SLS won't have the "twang" to deal with because its engines are axially mounted.
$endgroup$
– Organic Marble
1 hour ago
|
show 2 more comments
$begingroup$
A good assumption is that the startup sequence is very similar to the SSME. Here is some SSME startup data showing the time you asked about from the Rocketdyne Pocket Data Book. Eventually the SLS will be using RS-25Es which are somewhat different from the SSME, but my guess is that the start sequence won't change much if at all.
The hashed field is test experience, the solid lines are the ICD requirements.
$endgroup$
A good assumption is that the startup sequence is very similar to the SSME. Here is some SSME startup data showing the time you asked about from the Rocketdyne Pocket Data Book. Eventually the SLS will be using RS-25Es which are somewhat different from the SSME, but my guess is that the start sequence won't change much if at all.
The hashed field is test experience, the solid lines are the ICD requirements.
edited 3 hours ago
answered 3 hours ago
Organic MarbleOrganic Marble
58.2k3159249
58.2k3159249
$begingroup$
Awesome! Exactly what I was looking for! Thank you!
$endgroup$
– Mitch99
2 hours ago
$begingroup$
@Mitch99 Since you're new to the site: If this answer is what you were looking for, please mark it as correct by clicking the gray checkmark beside it. And upvote if you have a mind to.
$endgroup$
– Organic Marble
2 hours ago
$begingroup$
Got it, thanks!!
$endgroup$
– Mitch99
1 hour ago
$begingroup$
So - since it takes ~4 seconds to get them to 100% thrust, do they then ignite them at T -4:00 seconds, and they count T -0:00 the time all of them are roughly at 100%, the SRBs get lit, and it's a "mission start"?
$endgroup$
– Mitch99
1 hour ago
$begingroup$
I only know about shuttle, but there the start command was send at ~T-5 seconds, which gave time for the SSMEs to light, the "twang" to settle, and then the SRBs lit at, yes, T-0. SLS won't have the "twang" to deal with because its engines are axially mounted.
$endgroup$
– Organic Marble
1 hour ago
|
show 2 more comments
$begingroup$
Awesome! Exactly what I was looking for! Thank you!
$endgroup$
– Mitch99
2 hours ago
$begingroup$
@Mitch99 Since you're new to the site: If this answer is what you were looking for, please mark it as correct by clicking the gray checkmark beside it. And upvote if you have a mind to.
$endgroup$
– Organic Marble
2 hours ago
$begingroup$
Got it, thanks!!
$endgroup$
– Mitch99
1 hour ago
$begingroup$
So - since it takes ~4 seconds to get them to 100% thrust, do they then ignite them at T -4:00 seconds, and they count T -0:00 the time all of them are roughly at 100%, the SRBs get lit, and it's a "mission start"?
$endgroup$
– Mitch99
1 hour ago
$begingroup$
I only know about shuttle, but there the start command was send at ~T-5 seconds, which gave time for the SSMEs to light, the "twang" to settle, and then the SRBs lit at, yes, T-0. SLS won't have the "twang" to deal with because its engines are axially mounted.
$endgroup$
– Organic Marble
1 hour ago
$begingroup$
Awesome! Exactly what I was looking for! Thank you!
$endgroup$
– Mitch99
2 hours ago
$begingroup$
Awesome! Exactly what I was looking for! Thank you!
$endgroup$
– Mitch99
2 hours ago
$begingroup$
@Mitch99 Since you're new to the site: If this answer is what you were looking for, please mark it as correct by clicking the gray checkmark beside it. And upvote if you have a mind to.
$endgroup$
– Organic Marble
2 hours ago
$begingroup$
@Mitch99 Since you're new to the site: If this answer is what you were looking for, please mark it as correct by clicking the gray checkmark beside it. And upvote if you have a mind to.
$endgroup$
– Organic Marble
2 hours ago
$begingroup$
Got it, thanks!!
$endgroup$
– Mitch99
1 hour ago
$begingroup$
Got it, thanks!!
$endgroup$
– Mitch99
1 hour ago
$begingroup$
So - since it takes ~4 seconds to get them to 100% thrust, do they then ignite them at T -4:00 seconds, and they count T -0:00 the time all of them are roughly at 100%, the SRBs get lit, and it's a "mission start"?
$endgroup$
– Mitch99
1 hour ago
$begingroup$
So - since it takes ~4 seconds to get them to 100% thrust, do they then ignite them at T -4:00 seconds, and they count T -0:00 the time all of them are roughly at 100%, the SRBs get lit, and it's a "mission start"?
$endgroup$
– Mitch99
1 hour ago
$begingroup$
I only know about shuttle, but there the start command was send at ~T-5 seconds, which gave time for the SSMEs to light, the "twang" to settle, and then the SRBs lit at, yes, T-0. SLS won't have the "twang" to deal with because its engines are axially mounted.
$endgroup$
– Organic Marble
1 hour ago
$begingroup$
I only know about shuttle, but there the start command was send at ~T-5 seconds, which gave time for the SSMEs to light, the "twang" to settle, and then the SRBs lit at, yes, T-0. SLS won't have the "twang" to deal with because its engines are axially mounted.
$endgroup$
– Organic Marble
1 hour ago
|
show 2 more comments
Mitch99 is a new contributor. Be nice, and check out our Code of Conduct.
Mitch99 is a new contributor. Be nice, and check out our Code of Conduct.
Mitch99 is a new contributor. Be nice, and check out our Code of Conduct.
Mitch99 is a new contributor. Be nice, and check out our Code of Conduct.
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-engines, nasa, sls, ssme