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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?













2












$begingroup$


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!










share|improve this question









New contributor




Mitch99 is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
Check out our Code of Conduct.







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    2












    $begingroup$


    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!










    share|improve this question









    New contributor




    Mitch99 is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
    Check out our Code of Conduct.







    $endgroup$














      2












      2








      2





      $begingroup$


      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!










      share|improve this question









      New contributor




      Mitch99 is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
      Check out our Code of Conduct.







      $endgroup$




      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






      share|improve this question









      New contributor




      Mitch99 is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
      Check out our Code of Conduct.











      share|improve this question









      New contributor




      Mitch99 is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
      Check out our Code of Conduct.









      share|improve this question




      share|improve this question








      edited 2 hours ago









      Organic Marble

      58.2k3159249




      58.2k3159249






      New contributor




      Mitch99 is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
      Check out our Code of Conduct.









      asked 4 hours ago









      Mitch99Mitch99

      254




      254




      New contributor




      Mitch99 is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
      Check out our Code of Conduct.





      New contributor





      Mitch99 is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
      Check out our Code of Conduct.






      Mitch99 is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
      Check out our Code of Conduct.




















          1 Answer
          1






          active

          oldest

          votes


















          2












          $begingroup$

          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.



          enter image description here



          The hashed field is test experience, the solid lines are the ICD requirements.






          share|improve this answer











          $endgroup$












          • $begingroup$
            Awesome! Exactly what I was looking for! Thank you!
            $endgroup$
            – Mitch99
            1 hour 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
            1 hour ago











          • $begingroup$
            Got it, thanks!!
            $endgroup$
            – Mitch99
            51 mins 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
            42 mins 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
            40 mins ago










          Your Answer





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          1 Answer
          1






          active

          oldest

          votes








          1 Answer
          1






          active

          oldest

          votes









          active

          oldest

          votes






          active

          oldest

          votes









          2












          $begingroup$

          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.



          enter image description here



          The hashed field is test experience, the solid lines are the ICD requirements.






          share|improve this answer











          $endgroup$












          • $begingroup$
            Awesome! Exactly what I was looking for! Thank you!
            $endgroup$
            – Mitch99
            1 hour 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
            1 hour ago











          • $begingroup$
            Got it, thanks!!
            $endgroup$
            – Mitch99
            51 mins 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
            42 mins 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
            40 mins ago















          2












          $begingroup$

          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.



          enter image description here



          The hashed field is test experience, the solid lines are the ICD requirements.






          share|improve this answer











          $endgroup$












          • $begingroup$
            Awesome! Exactly what I was looking for! Thank you!
            $endgroup$
            – Mitch99
            1 hour 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
            1 hour ago











          • $begingroup$
            Got it, thanks!!
            $endgroup$
            – Mitch99
            51 mins 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
            42 mins 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
            40 mins ago













          2












          2








          2





          $begingroup$

          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.



          enter image description here



          The hashed field is test experience, the solid lines are the ICD requirements.






          share|improve this answer











          $endgroup$



          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.



          enter image description here



          The hashed field is test experience, the solid lines are the ICD requirements.







          share|improve this answer














          share|improve this answer



          share|improve this answer








          edited 2 hours ago

























          answered 2 hours ago









          Organic MarbleOrganic Marble

          58.2k3159249




          58.2k3159249











          • $begingroup$
            Awesome! Exactly what I was looking for! Thank you!
            $endgroup$
            – Mitch99
            1 hour 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
            1 hour ago











          • $begingroup$
            Got it, thanks!!
            $endgroup$
            – Mitch99
            51 mins 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
            42 mins 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
            40 mins ago
















          • $begingroup$
            Awesome! Exactly what I was looking for! Thank you!
            $endgroup$
            – Mitch99
            1 hour 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
            1 hour ago











          • $begingroup$
            Got it, thanks!!
            $endgroup$
            – Mitch99
            51 mins 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
            42 mins 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
            40 mins ago















          $begingroup$
          Awesome! Exactly what I was looking for! Thank you!
          $endgroup$
          – Mitch99
          1 hour ago




          $begingroup$
          Awesome! Exactly what I was looking for! Thank you!
          $endgroup$
          – Mitch99
          1 hour 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
          1 hour 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
          1 hour ago













          $begingroup$
          Got it, thanks!!
          $endgroup$
          – Mitch99
          51 mins ago




          $begingroup$
          Got it, thanks!!
          $endgroup$
          – Mitch99
          51 mins 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
          42 mins 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
          42 mins 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
          40 mins 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
          40 mins ago










          Mitch99 is a new contributor. Be nice, and check out our Code of Conduct.









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