What are the pros and cons of Aerospike nosecones?Just how pointy does a rocket's nosecone need to be?Are ICBMs and orbital launchers similar enough to be co-developed today?What kind of missions are US surplus ICBM's capable of launching?What was the death toll of the Nedelin catastrophe?What are these tiny triangular fins on the Soyuz launcher?Why not jettison the nose-cone from Falcon Heavy side boosters for better control authority?Why are the bottom of most stages flat?What are these circular structures around the rocket?What would a “Kármán plane” look like, a bird, or a plane?What causes a rocket to be destroyed during launch other than leaking fuel?Why does in-flight mission abort often ends in ballistic high-g reentry?

Examples of proofs by making reduction to a finite set

What is the meaning of "order" in this quote?

How to give my students a straightedge instead of a ruler

Is it possible to determine the index of a bip32 address?

Seven Places at Once - Another Google Earth Challenge?

Why is it called a stateful and a stateless firewall?

Wrong Schengen Visa exit stamp on my passport, who can I complain to?

Where is it? - The Google Earth Challenge Ep. 3

Block diagram vs flow chart?

In what sequence should an advanced civilization teach technology to medieval society to maximize rate of adoption?

Python web-scraper to download table of transistor counts from Wikipedia

Is it appropriate to CC a lot of people on an email

Importance of the current postdoc advisor's letter in TT job search

Are space camera sensors usually round, or square?

'Overwrote' files, space still occupied, are they lost?

Insight into cavity resonators

What are the advantages and disadvantages of tail wheels that cause modern airplanes to not use them?

Read string of any length in C

Asked to Not Use Transactions and to Use A Workaround to Simulate One

Building Truncatable Primes using Nest(List), While, Fold

How to be sure services and researches offered by the University are not becoming cases of unfair competition?

Can derivatives be defined as anti-integrals?

Shouldn't countries like Russia and Canada support global warming?

Teleport everything in a large zone; or teleport all living things and make a lot of equipment disappear



What are the pros and cons of Aerospike nosecones?


Just how pointy does a rocket's nosecone need to be?Are ICBMs and orbital launchers similar enough to be co-developed today?What kind of missions are US surplus ICBM's capable of launching?What was the death toll of the Nedelin catastrophe?What are these tiny triangular fins on the Soyuz launcher?Why not jettison the nose-cone from Falcon Heavy side boosters for better control authority?Why are the bottom of most stages flat?What are these circular structures around the rocket?What would a “Kármán plane” look like, a bird, or a plane?What causes a rocket to be destroyed during launch other than leaking fuel?Why does in-flight mission abort often ends in ballistic high-g reentry?






.everyoneloves__top-leaderboard:empty,.everyoneloves__mid-leaderboard:empty,.everyoneloves__bot-mid-leaderboard:empty margin-bottom:0;








24












$begingroup$


Some rockets, mainly (only?) ICBMs have Aerospike nosecones



Why are they preferred in lieu of traditional nose cones?



Illustrations:



enter image description here An aerospike nosecone on a trident ICBM



Video including the spike in flight deployment of a M51 ICBM:















share|improve this question











$endgroup$




















    24












    $begingroup$


    Some rockets, mainly (only?) ICBMs have Aerospike nosecones



    Why are they preferred in lieu of traditional nose cones?



    Illustrations:



    enter image description here An aerospike nosecone on a trident ICBM



    Video including the spike in flight deployment of a M51 ICBM:















    share|improve this question











    $endgroup$
















      24












      24








      24





      $begingroup$


      Some rockets, mainly (only?) ICBMs have Aerospike nosecones



      Why are they preferred in lieu of traditional nose cones?



      Illustrations:



      enter image description here An aerospike nosecone on a trident ICBM



      Video including the spike in flight deployment of a M51 ICBM:















      share|improve this question











      $endgroup$




      Some rockets, mainly (only?) ICBMs have Aerospike nosecones



      Why are they preferred in lieu of traditional nose cones?



      Illustrations:



      enter image description here An aerospike nosecone on a trident ICBM



      Video including the spike in flight deployment of a M51 ICBM:




















      aerodynamics icbm nosecone






      share|improve this question















      share|improve this question













      share|improve this question




      share|improve this question








      edited May 22 at 17:04









      Magic Octopus Urn

      4,5681 gold badge19 silver badges62 bronze badges




      4,5681 gold badge19 silver badges62 bronze badges










      asked Apr 15 at 9:04









      AntziAntzi

      9,0041 gold badge29 silver badges60 bronze badges




      9,0041 gold badge29 silver badges60 bronze badges























          2 Answers
          2






          active

          oldest

          votes


















          48














          $begingroup$

          Aerospike nosecones have a couple of big benefits which, to fully appreciate, I'd need to give a little background on.



          At the risk of dating myself, "Sherman, set the WABAC machine to the 1950s":



          The United States had a problem. It was trying to develop a missile with a range of 1,000 miles based on the work of Wernher von Braun and a number of other German scientists after the war. It was widely recognized that the most efficient way to get a missile to travel with that kind of range was to launch it out of the Earth's atmosphere up into space and have it re-enter the atmosphere at its desired impact point. However, whenever they tried to re-enter anything from an altitude above about 100 miles, it would melt from the friction of air moving over it. Conventional wisdom told everyone that the answer was to make the nosecone more streamlined - that is, make it longer, sharper, like a bullet. But no matter how sharp or streamlined they tried to make it, the nosecone kept melting.



          But then, H. Julian "Harvey" Allen came along. He was one of the greatest engineers of our time and fit pretty much every stereotype about engineers. He was odd, enthusiastic, random in his thinking, and brilliant. And Harvey had an idea:



          If the nosecones kept melting because of the extreme friction, then maybe the answer was to make it less streamlined. He floated the idea of making the nosecone look like a "Civil War cannonball." He and his colleagues ran the numbers and published a paper in 1953 that stated "Not only should pointed bodies be avoided, but the rounded nosecone should have as large a radius as possible." By having a large, round nosecone, your body develops an extremely turbulent boundary layer on its leading edge. This boundary layer actually ends up with a fairly stable temperature and protects your body from the excessive heat of re-entry.



          Wind tunnel tests of different nosecone geometries



          By 1955, the Air Force had adopted Harvey's idea and developed the Atlas ICBM.



          Ok, so let's fast-forward to the 1970s and the introduction of the aerospike. As a body approaches and exceeds Mach 1, it experiences a tremendous amount of heat and turbulence. It's really difficult to maneuver and control something in an environment that intense. Well, we knew from back in the 1950s that missiles needed round nosecones to reduce friction and aerodynamic heating, but we also knew that we needed pointy, streamlined bodies to reduce drag and conserve fuel when leaving the atmosphere. Adding an aerospike to a big, round nosecone is a great solution that gave you the best of both worlds! The aerospike pierces the air in front of the body and displaces the shockwave, reducing drag and friction/pressure changes around the body itself.



          Aerospike Wind Tunnel Test



          There are further benefits to an aerospike which might one day allow for supersonic travel over the continental U.S. (something which is currently banned due to - mostly - noise). By having a long aerospike, you can create multiple small shockwaves instead of one very large shockwave. It's the keynote feature of the "Quiet Supersonic Jet". That's less applicable to your question about ICBMs - it's just more of a fun tidbit that I wanted to toss in there since I did some work on the QSJ a few years ago.






          share|improve this answer











          $endgroup$










          • 5




            $begingroup$
            The round nosecone that the aerospike sticks out of is not the reentry body, so your sentence "Adding an aerospike to a big, round nosecone is a great solution to that problem." doesn't make much sense. The reentry vehicles are rounded cones hidden under that nosecone. i0.wp.com/www.llquakers.org.uk/hemel/web/wp-content/uploads/… What we see as the nosecone at launch is jettisoned before entry and the reentry vehicles are deployed. The rounded nosecone with aerospike is specifically an ascent design and has nothing to do with entry.
            $endgroup$
            – Organic Marble
            Apr 15 at 16:10







          • 2




            $begingroup$
            @OrganicMarble You're absolutely right, I worded that terribly! Made some edits and added some pictures. Thanks for the feedback!
            $endgroup$
            – Steve
            Apr 15 at 16:32






          • 2




            $begingroup$
            Interesting! How quiet can you make a supersonic jet with those? (Maybe this should be a question on Aviation?)
            $endgroup$
            – Eth
            Apr 15 at 17:44






          • 2




            $begingroup$
            @Eth they can get pretty quiet. The latest projections I heard were around 60-70 dB or so. The Concorde's sonic boom was in the 110 dB range so this would be somewhere between 15-30 times quieter.
            $endgroup$
            – Steve
            Apr 15 at 18:43






          • 1




            $begingroup$
            Note that it's not generally "friction" that causes the majority of the heating, but rather compression of the air. But for the purposes of your answer, keeping the boundary layer as far from the skin as possible helps with both sources.
            $endgroup$
            – Perkins
            Apr 15 at 23:13


















          21














          $begingroup$

          You'll notice it is used on submarine launched ICBMs.
          Blunt noses are very efficient for the missile to get out of water (and are shorter than long, profiled ones, which helps with submarine diameter), but aren't great in atmosphere; hence the deployable aerospike to make them efficient in both media.






          share|improve this answer











          $endgroup$










          • 5




            $begingroup$
            The Trident, specifically, had to fit in the Poseiden-sized launch tubes which it was replacing, and carried an extra stage over the Poseiden. The deployable aerospike was the only available solution given the space constraints - there are other nose cone designs which would have been suitable but there was no room to fit them into the Trident design.
            $endgroup$
            – J...
            Apr 15 at 14:48













          Your Answer








          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/4.0/"u003ecc by-sa 4.0 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
          );



          );














          draft saved

          draft discarded
















          StackExchange.ready(
          function ()
          StackExchange.openid.initPostLogin('.new-post-login', 'https%3a%2f%2fspace.stackexchange.com%2fquestions%2f35523%2fwhat-are-the-pros-and-cons-of-aerospike-nosecones%23new-answer', 'question_page');

          );

          Post as a guest















          Required, but never shown

























          2 Answers
          2






          active

          oldest

          votes








          2 Answers
          2






          active

          oldest

          votes









          active

          oldest

          votes






          active

          oldest

          votes









          48














          $begingroup$

          Aerospike nosecones have a couple of big benefits which, to fully appreciate, I'd need to give a little background on.



          At the risk of dating myself, "Sherman, set the WABAC machine to the 1950s":



          The United States had a problem. It was trying to develop a missile with a range of 1,000 miles based on the work of Wernher von Braun and a number of other German scientists after the war. It was widely recognized that the most efficient way to get a missile to travel with that kind of range was to launch it out of the Earth's atmosphere up into space and have it re-enter the atmosphere at its desired impact point. However, whenever they tried to re-enter anything from an altitude above about 100 miles, it would melt from the friction of air moving over it. Conventional wisdom told everyone that the answer was to make the nosecone more streamlined - that is, make it longer, sharper, like a bullet. But no matter how sharp or streamlined they tried to make it, the nosecone kept melting.



          But then, H. Julian "Harvey" Allen came along. He was one of the greatest engineers of our time and fit pretty much every stereotype about engineers. He was odd, enthusiastic, random in his thinking, and brilliant. And Harvey had an idea:



          If the nosecones kept melting because of the extreme friction, then maybe the answer was to make it less streamlined. He floated the idea of making the nosecone look like a "Civil War cannonball." He and his colleagues ran the numbers and published a paper in 1953 that stated "Not only should pointed bodies be avoided, but the rounded nosecone should have as large a radius as possible." By having a large, round nosecone, your body develops an extremely turbulent boundary layer on its leading edge. This boundary layer actually ends up with a fairly stable temperature and protects your body from the excessive heat of re-entry.



          Wind tunnel tests of different nosecone geometries



          By 1955, the Air Force had adopted Harvey's idea and developed the Atlas ICBM.



          Ok, so let's fast-forward to the 1970s and the introduction of the aerospike. As a body approaches and exceeds Mach 1, it experiences a tremendous amount of heat and turbulence. It's really difficult to maneuver and control something in an environment that intense. Well, we knew from back in the 1950s that missiles needed round nosecones to reduce friction and aerodynamic heating, but we also knew that we needed pointy, streamlined bodies to reduce drag and conserve fuel when leaving the atmosphere. Adding an aerospike to a big, round nosecone is a great solution that gave you the best of both worlds! The aerospike pierces the air in front of the body and displaces the shockwave, reducing drag and friction/pressure changes around the body itself.



          Aerospike Wind Tunnel Test



          There are further benefits to an aerospike which might one day allow for supersonic travel over the continental U.S. (something which is currently banned due to - mostly - noise). By having a long aerospike, you can create multiple small shockwaves instead of one very large shockwave. It's the keynote feature of the "Quiet Supersonic Jet". That's less applicable to your question about ICBMs - it's just more of a fun tidbit that I wanted to toss in there since I did some work on the QSJ a few years ago.






          share|improve this answer











          $endgroup$










          • 5




            $begingroup$
            The round nosecone that the aerospike sticks out of is not the reentry body, so your sentence "Adding an aerospike to a big, round nosecone is a great solution to that problem." doesn't make much sense. The reentry vehicles are rounded cones hidden under that nosecone. i0.wp.com/www.llquakers.org.uk/hemel/web/wp-content/uploads/… What we see as the nosecone at launch is jettisoned before entry and the reentry vehicles are deployed. The rounded nosecone with aerospike is specifically an ascent design and has nothing to do with entry.
            $endgroup$
            – Organic Marble
            Apr 15 at 16:10







          • 2




            $begingroup$
            @OrganicMarble You're absolutely right, I worded that terribly! Made some edits and added some pictures. Thanks for the feedback!
            $endgroup$
            – Steve
            Apr 15 at 16:32






          • 2




            $begingroup$
            Interesting! How quiet can you make a supersonic jet with those? (Maybe this should be a question on Aviation?)
            $endgroup$
            – Eth
            Apr 15 at 17:44






          • 2




            $begingroup$
            @Eth they can get pretty quiet. The latest projections I heard were around 60-70 dB or so. The Concorde's sonic boom was in the 110 dB range so this would be somewhere between 15-30 times quieter.
            $endgroup$
            – Steve
            Apr 15 at 18:43






          • 1




            $begingroup$
            Note that it's not generally "friction" that causes the majority of the heating, but rather compression of the air. But for the purposes of your answer, keeping the boundary layer as far from the skin as possible helps with both sources.
            $endgroup$
            – Perkins
            Apr 15 at 23:13















          48














          $begingroup$

          Aerospike nosecones have a couple of big benefits which, to fully appreciate, I'd need to give a little background on.



          At the risk of dating myself, "Sherman, set the WABAC machine to the 1950s":



          The United States had a problem. It was trying to develop a missile with a range of 1,000 miles based on the work of Wernher von Braun and a number of other German scientists after the war. It was widely recognized that the most efficient way to get a missile to travel with that kind of range was to launch it out of the Earth's atmosphere up into space and have it re-enter the atmosphere at its desired impact point. However, whenever they tried to re-enter anything from an altitude above about 100 miles, it would melt from the friction of air moving over it. Conventional wisdom told everyone that the answer was to make the nosecone more streamlined - that is, make it longer, sharper, like a bullet. But no matter how sharp or streamlined they tried to make it, the nosecone kept melting.



          But then, H. Julian "Harvey" Allen came along. He was one of the greatest engineers of our time and fit pretty much every stereotype about engineers. He was odd, enthusiastic, random in his thinking, and brilliant. And Harvey had an idea:



          If the nosecones kept melting because of the extreme friction, then maybe the answer was to make it less streamlined. He floated the idea of making the nosecone look like a "Civil War cannonball." He and his colleagues ran the numbers and published a paper in 1953 that stated "Not only should pointed bodies be avoided, but the rounded nosecone should have as large a radius as possible." By having a large, round nosecone, your body develops an extremely turbulent boundary layer on its leading edge. This boundary layer actually ends up with a fairly stable temperature and protects your body from the excessive heat of re-entry.



          Wind tunnel tests of different nosecone geometries



          By 1955, the Air Force had adopted Harvey's idea and developed the Atlas ICBM.



          Ok, so let's fast-forward to the 1970s and the introduction of the aerospike. As a body approaches and exceeds Mach 1, it experiences a tremendous amount of heat and turbulence. It's really difficult to maneuver and control something in an environment that intense. Well, we knew from back in the 1950s that missiles needed round nosecones to reduce friction and aerodynamic heating, but we also knew that we needed pointy, streamlined bodies to reduce drag and conserve fuel when leaving the atmosphere. Adding an aerospike to a big, round nosecone is a great solution that gave you the best of both worlds! The aerospike pierces the air in front of the body and displaces the shockwave, reducing drag and friction/pressure changes around the body itself.



          Aerospike Wind Tunnel Test



          There are further benefits to an aerospike which might one day allow for supersonic travel over the continental U.S. (something which is currently banned due to - mostly - noise). By having a long aerospike, you can create multiple small shockwaves instead of one very large shockwave. It's the keynote feature of the "Quiet Supersonic Jet". That's less applicable to your question about ICBMs - it's just more of a fun tidbit that I wanted to toss in there since I did some work on the QSJ a few years ago.






          share|improve this answer











          $endgroup$










          • 5




            $begingroup$
            The round nosecone that the aerospike sticks out of is not the reentry body, so your sentence "Adding an aerospike to a big, round nosecone is a great solution to that problem." doesn't make much sense. The reentry vehicles are rounded cones hidden under that nosecone. i0.wp.com/www.llquakers.org.uk/hemel/web/wp-content/uploads/… What we see as the nosecone at launch is jettisoned before entry and the reentry vehicles are deployed. The rounded nosecone with aerospike is specifically an ascent design and has nothing to do with entry.
            $endgroup$
            – Organic Marble
            Apr 15 at 16:10







          • 2




            $begingroup$
            @OrganicMarble You're absolutely right, I worded that terribly! Made some edits and added some pictures. Thanks for the feedback!
            $endgroup$
            – Steve
            Apr 15 at 16:32






          • 2




            $begingroup$
            Interesting! How quiet can you make a supersonic jet with those? (Maybe this should be a question on Aviation?)
            $endgroup$
            – Eth
            Apr 15 at 17:44






          • 2




            $begingroup$
            @Eth they can get pretty quiet. The latest projections I heard were around 60-70 dB or so. The Concorde's sonic boom was in the 110 dB range so this would be somewhere between 15-30 times quieter.
            $endgroup$
            – Steve
            Apr 15 at 18:43






          • 1




            $begingroup$
            Note that it's not generally "friction" that causes the majority of the heating, but rather compression of the air. But for the purposes of your answer, keeping the boundary layer as far from the skin as possible helps with both sources.
            $endgroup$
            – Perkins
            Apr 15 at 23:13













          48














          48










          48







          $begingroup$

          Aerospike nosecones have a couple of big benefits which, to fully appreciate, I'd need to give a little background on.



          At the risk of dating myself, "Sherman, set the WABAC machine to the 1950s":



          The United States had a problem. It was trying to develop a missile with a range of 1,000 miles based on the work of Wernher von Braun and a number of other German scientists after the war. It was widely recognized that the most efficient way to get a missile to travel with that kind of range was to launch it out of the Earth's atmosphere up into space and have it re-enter the atmosphere at its desired impact point. However, whenever they tried to re-enter anything from an altitude above about 100 miles, it would melt from the friction of air moving over it. Conventional wisdom told everyone that the answer was to make the nosecone more streamlined - that is, make it longer, sharper, like a bullet. But no matter how sharp or streamlined they tried to make it, the nosecone kept melting.



          But then, H. Julian "Harvey" Allen came along. He was one of the greatest engineers of our time and fit pretty much every stereotype about engineers. He was odd, enthusiastic, random in his thinking, and brilliant. And Harvey had an idea:



          If the nosecones kept melting because of the extreme friction, then maybe the answer was to make it less streamlined. He floated the idea of making the nosecone look like a "Civil War cannonball." He and his colleagues ran the numbers and published a paper in 1953 that stated "Not only should pointed bodies be avoided, but the rounded nosecone should have as large a radius as possible." By having a large, round nosecone, your body develops an extremely turbulent boundary layer on its leading edge. This boundary layer actually ends up with a fairly stable temperature and protects your body from the excessive heat of re-entry.



          Wind tunnel tests of different nosecone geometries



          By 1955, the Air Force had adopted Harvey's idea and developed the Atlas ICBM.



          Ok, so let's fast-forward to the 1970s and the introduction of the aerospike. As a body approaches and exceeds Mach 1, it experiences a tremendous amount of heat and turbulence. It's really difficult to maneuver and control something in an environment that intense. Well, we knew from back in the 1950s that missiles needed round nosecones to reduce friction and aerodynamic heating, but we also knew that we needed pointy, streamlined bodies to reduce drag and conserve fuel when leaving the atmosphere. Adding an aerospike to a big, round nosecone is a great solution that gave you the best of both worlds! The aerospike pierces the air in front of the body and displaces the shockwave, reducing drag and friction/pressure changes around the body itself.



          Aerospike Wind Tunnel Test



          There are further benefits to an aerospike which might one day allow for supersonic travel over the continental U.S. (something which is currently banned due to - mostly - noise). By having a long aerospike, you can create multiple small shockwaves instead of one very large shockwave. It's the keynote feature of the "Quiet Supersonic Jet". That's less applicable to your question about ICBMs - it's just more of a fun tidbit that I wanted to toss in there since I did some work on the QSJ a few years ago.






          share|improve this answer











          $endgroup$



          Aerospike nosecones have a couple of big benefits which, to fully appreciate, I'd need to give a little background on.



          At the risk of dating myself, "Sherman, set the WABAC machine to the 1950s":



          The United States had a problem. It was trying to develop a missile with a range of 1,000 miles based on the work of Wernher von Braun and a number of other German scientists after the war. It was widely recognized that the most efficient way to get a missile to travel with that kind of range was to launch it out of the Earth's atmosphere up into space and have it re-enter the atmosphere at its desired impact point. However, whenever they tried to re-enter anything from an altitude above about 100 miles, it would melt from the friction of air moving over it. Conventional wisdom told everyone that the answer was to make the nosecone more streamlined - that is, make it longer, sharper, like a bullet. But no matter how sharp or streamlined they tried to make it, the nosecone kept melting.



          But then, H. Julian "Harvey" Allen came along. He was one of the greatest engineers of our time and fit pretty much every stereotype about engineers. He was odd, enthusiastic, random in his thinking, and brilliant. And Harvey had an idea:



          If the nosecones kept melting because of the extreme friction, then maybe the answer was to make it less streamlined. He floated the idea of making the nosecone look like a "Civil War cannonball." He and his colleagues ran the numbers and published a paper in 1953 that stated "Not only should pointed bodies be avoided, but the rounded nosecone should have as large a radius as possible." By having a large, round nosecone, your body develops an extremely turbulent boundary layer on its leading edge. This boundary layer actually ends up with a fairly stable temperature and protects your body from the excessive heat of re-entry.



          Wind tunnel tests of different nosecone geometries



          By 1955, the Air Force had adopted Harvey's idea and developed the Atlas ICBM.



          Ok, so let's fast-forward to the 1970s and the introduction of the aerospike. As a body approaches and exceeds Mach 1, it experiences a tremendous amount of heat and turbulence. It's really difficult to maneuver and control something in an environment that intense. Well, we knew from back in the 1950s that missiles needed round nosecones to reduce friction and aerodynamic heating, but we also knew that we needed pointy, streamlined bodies to reduce drag and conserve fuel when leaving the atmosphere. Adding an aerospike to a big, round nosecone is a great solution that gave you the best of both worlds! The aerospike pierces the air in front of the body and displaces the shockwave, reducing drag and friction/pressure changes around the body itself.



          Aerospike Wind Tunnel Test



          There are further benefits to an aerospike which might one day allow for supersonic travel over the continental U.S. (something which is currently banned due to - mostly - noise). By having a long aerospike, you can create multiple small shockwaves instead of one very large shockwave. It's the keynote feature of the "Quiet Supersonic Jet". That's less applicable to your question about ICBMs - it's just more of a fun tidbit that I wanted to toss in there since I did some work on the QSJ a few years ago.







          share|improve this answer














          share|improve this answer



          share|improve this answer








          edited Sep 9 at 13:24

























          answered Apr 15 at 15:35









          SteveSteve

          5862 silver badges5 bronze badges




          5862 silver badges5 bronze badges










          • 5




            $begingroup$
            The round nosecone that the aerospike sticks out of is not the reentry body, so your sentence "Adding an aerospike to a big, round nosecone is a great solution to that problem." doesn't make much sense. The reentry vehicles are rounded cones hidden under that nosecone. i0.wp.com/www.llquakers.org.uk/hemel/web/wp-content/uploads/… What we see as the nosecone at launch is jettisoned before entry and the reentry vehicles are deployed. The rounded nosecone with aerospike is specifically an ascent design and has nothing to do with entry.
            $endgroup$
            – Organic Marble
            Apr 15 at 16:10







          • 2




            $begingroup$
            @OrganicMarble You're absolutely right, I worded that terribly! Made some edits and added some pictures. Thanks for the feedback!
            $endgroup$
            – Steve
            Apr 15 at 16:32






          • 2




            $begingroup$
            Interesting! How quiet can you make a supersonic jet with those? (Maybe this should be a question on Aviation?)
            $endgroup$
            – Eth
            Apr 15 at 17:44






          • 2




            $begingroup$
            @Eth they can get pretty quiet. The latest projections I heard were around 60-70 dB or so. The Concorde's sonic boom was in the 110 dB range so this would be somewhere between 15-30 times quieter.
            $endgroup$
            – Steve
            Apr 15 at 18:43






          • 1




            $begingroup$
            Note that it's not generally "friction" that causes the majority of the heating, but rather compression of the air. But for the purposes of your answer, keeping the boundary layer as far from the skin as possible helps with both sources.
            $endgroup$
            – Perkins
            Apr 15 at 23:13












          • 5




            $begingroup$
            The round nosecone that the aerospike sticks out of is not the reentry body, so your sentence "Adding an aerospike to a big, round nosecone is a great solution to that problem." doesn't make much sense. The reentry vehicles are rounded cones hidden under that nosecone. i0.wp.com/www.llquakers.org.uk/hemel/web/wp-content/uploads/… What we see as the nosecone at launch is jettisoned before entry and the reentry vehicles are deployed. The rounded nosecone with aerospike is specifically an ascent design and has nothing to do with entry.
            $endgroup$
            – Organic Marble
            Apr 15 at 16:10







          • 2




            $begingroup$
            @OrganicMarble You're absolutely right, I worded that terribly! Made some edits and added some pictures. Thanks for the feedback!
            $endgroup$
            – Steve
            Apr 15 at 16:32






          • 2




            $begingroup$
            Interesting! How quiet can you make a supersonic jet with those? (Maybe this should be a question on Aviation?)
            $endgroup$
            – Eth
            Apr 15 at 17:44






          • 2




            $begingroup$
            @Eth they can get pretty quiet. The latest projections I heard were around 60-70 dB or so. The Concorde's sonic boom was in the 110 dB range so this would be somewhere between 15-30 times quieter.
            $endgroup$
            – Steve
            Apr 15 at 18:43






          • 1




            $begingroup$
            Note that it's not generally "friction" that causes the majority of the heating, but rather compression of the air. But for the purposes of your answer, keeping the boundary layer as far from the skin as possible helps with both sources.
            $endgroup$
            – Perkins
            Apr 15 at 23:13







          5




          5




          $begingroup$
          The round nosecone that the aerospike sticks out of is not the reentry body, so your sentence "Adding an aerospike to a big, round nosecone is a great solution to that problem." doesn't make much sense. The reentry vehicles are rounded cones hidden under that nosecone. i0.wp.com/www.llquakers.org.uk/hemel/web/wp-content/uploads/… What we see as the nosecone at launch is jettisoned before entry and the reentry vehicles are deployed. The rounded nosecone with aerospike is specifically an ascent design and has nothing to do with entry.
          $endgroup$
          – Organic Marble
          Apr 15 at 16:10





          $begingroup$
          The round nosecone that the aerospike sticks out of is not the reentry body, so your sentence "Adding an aerospike to a big, round nosecone is a great solution to that problem." doesn't make much sense. The reentry vehicles are rounded cones hidden under that nosecone. i0.wp.com/www.llquakers.org.uk/hemel/web/wp-content/uploads/… What we see as the nosecone at launch is jettisoned before entry and the reentry vehicles are deployed. The rounded nosecone with aerospike is specifically an ascent design and has nothing to do with entry.
          $endgroup$
          – Organic Marble
          Apr 15 at 16:10





          2




          2




          $begingroup$
          @OrganicMarble You're absolutely right, I worded that terribly! Made some edits and added some pictures. Thanks for the feedback!
          $endgroup$
          – Steve
          Apr 15 at 16:32




          $begingroup$
          @OrganicMarble You're absolutely right, I worded that terribly! Made some edits and added some pictures. Thanks for the feedback!
          $endgroup$
          – Steve
          Apr 15 at 16:32




          2




          2




          $begingroup$
          Interesting! How quiet can you make a supersonic jet with those? (Maybe this should be a question on Aviation?)
          $endgroup$
          – Eth
          Apr 15 at 17:44




          $begingroup$
          Interesting! How quiet can you make a supersonic jet with those? (Maybe this should be a question on Aviation?)
          $endgroup$
          – Eth
          Apr 15 at 17:44




          2




          2




          $begingroup$
          @Eth they can get pretty quiet. The latest projections I heard were around 60-70 dB or so. The Concorde's sonic boom was in the 110 dB range so this would be somewhere between 15-30 times quieter.
          $endgroup$
          – Steve
          Apr 15 at 18:43




          $begingroup$
          @Eth they can get pretty quiet. The latest projections I heard were around 60-70 dB or so. The Concorde's sonic boom was in the 110 dB range so this would be somewhere between 15-30 times quieter.
          $endgroup$
          – Steve
          Apr 15 at 18:43




          1




          1




          $begingroup$
          Note that it's not generally "friction" that causes the majority of the heating, but rather compression of the air. But for the purposes of your answer, keeping the boundary layer as far from the skin as possible helps with both sources.
          $endgroup$
          – Perkins
          Apr 15 at 23:13




          $begingroup$
          Note that it's not generally "friction" that causes the majority of the heating, but rather compression of the air. But for the purposes of your answer, keeping the boundary layer as far from the skin as possible helps with both sources.
          $endgroup$
          – Perkins
          Apr 15 at 23:13













          21














          $begingroup$

          You'll notice it is used on submarine launched ICBMs.
          Blunt noses are very efficient for the missile to get out of water (and are shorter than long, profiled ones, which helps with submarine diameter), but aren't great in atmosphere; hence the deployable aerospike to make them efficient in both media.






          share|improve this answer











          $endgroup$










          • 5




            $begingroup$
            The Trident, specifically, had to fit in the Poseiden-sized launch tubes which it was replacing, and carried an extra stage over the Poseiden. The deployable aerospike was the only available solution given the space constraints - there are other nose cone designs which would have been suitable but there was no room to fit them into the Trident design.
            $endgroup$
            – J...
            Apr 15 at 14:48















          21














          $begingroup$

          You'll notice it is used on submarine launched ICBMs.
          Blunt noses are very efficient for the missile to get out of water (and are shorter than long, profiled ones, which helps with submarine diameter), but aren't great in atmosphere; hence the deployable aerospike to make them efficient in both media.






          share|improve this answer











          $endgroup$










          • 5




            $begingroup$
            The Trident, specifically, had to fit in the Poseiden-sized launch tubes which it was replacing, and carried an extra stage over the Poseiden. The deployable aerospike was the only available solution given the space constraints - there are other nose cone designs which would have been suitable but there was no room to fit them into the Trident design.
            $endgroup$
            – J...
            Apr 15 at 14:48













          21














          21










          21







          $begingroup$

          You'll notice it is used on submarine launched ICBMs.
          Blunt noses are very efficient for the missile to get out of water (and are shorter than long, profiled ones, which helps with submarine diameter), but aren't great in atmosphere; hence the deployable aerospike to make them efficient in both media.






          share|improve this answer











          $endgroup$



          You'll notice it is used on submarine launched ICBMs.
          Blunt noses are very efficient for the missile to get out of water (and are shorter than long, profiled ones, which helps with submarine diameter), but aren't great in atmosphere; hence the deployable aerospike to make them efficient in both media.







          share|improve this answer














          share|improve this answer



          share|improve this answer








          edited Apr 15 at 14:08









          user23432

          2061 silver badge4 bronze badges




          2061 silver badge4 bronze badges










          answered Apr 15 at 9:40









          KhayKhay

          2112 bronze badges




          2112 bronze badges










          • 5




            $begingroup$
            The Trident, specifically, had to fit in the Poseiden-sized launch tubes which it was replacing, and carried an extra stage over the Poseiden. The deployable aerospike was the only available solution given the space constraints - there are other nose cone designs which would have been suitable but there was no room to fit them into the Trident design.
            $endgroup$
            – J...
            Apr 15 at 14:48












          • 5




            $begingroup$
            The Trident, specifically, had to fit in the Poseiden-sized launch tubes which it was replacing, and carried an extra stage over the Poseiden. The deployable aerospike was the only available solution given the space constraints - there are other nose cone designs which would have been suitable but there was no room to fit them into the Trident design.
            $endgroup$
            – J...
            Apr 15 at 14:48







          5




          5




          $begingroup$
          The Trident, specifically, had to fit in the Poseiden-sized launch tubes which it was replacing, and carried an extra stage over the Poseiden. The deployable aerospike was the only available solution given the space constraints - there are other nose cone designs which would have been suitable but there was no room to fit them into the Trident design.
          $endgroup$
          – J...
          Apr 15 at 14:48




          $begingroup$
          The Trident, specifically, had to fit in the Poseiden-sized launch tubes which it was replacing, and carried an extra stage over the Poseiden. The deployable aerospike was the only available solution given the space constraints - there are other nose cone designs which would have been suitable but there was no room to fit them into the Trident design.
          $endgroup$
          – J...
          Apr 15 at 14:48


















          draft saved

          draft discarded















































          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.




          draft saved


          draft discarded














          StackExchange.ready(
          function ()
          StackExchange.openid.initPostLogin('.new-post-login', 'https%3a%2f%2fspace.stackexchange.com%2fquestions%2f35523%2fwhat-are-the-pros-and-cons-of-aerospike-nosecones%23new-answer', 'question_page');

          );

          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







          Popular posts from this blog

          Tamil (spriik) Luke uk diar | Nawigatjuun

          Align equal signs while including text over equalitiesAMS align: left aligned text/math plus multicolumn alignmentMultiple alignmentsAligning equations in multiple placesNumbering and aligning an equation with multiple columnsHow to align one equation with another multline equationUsing \ in environments inside the begintabularxNumber equations and preserving alignment of equal signsHow can I align equations to the left and to the right?Double equation alignment problem within align enviromentAligned within align: Why are they right-aligned?

          Training a classifier when some of the features are unknownWhy does Gradient Boosting regression predict negative values when there are no negative y-values in my training set?How to improve an existing (trained) classifier?What is effect when I set up some self defined predisctor variables?Why Matlab neural network classification returns decimal values on prediction dataset?Fitting and transforming text data in training, testing, and validation setsHow to quantify the performance of the classifier (multi-class SVM) using the test data?How do I control for some patients providing multiple samples in my training data?Training and Test setTraining a convolutional neural network for image denoising in MatlabShouldn't an autoencoder with #(neurons in hidden layer) = #(neurons in input layer) be “perfect”?