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In all rockets that launch satellites to orbit, the satellite is always placed at the top.

Why are payloads always placed at the top of rockets?

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    $\begingroup$ For a moment, you got me stumped :) Actually, payload can be placed at the side, so your premise is false. One thing I won't do is place the sat UNDER the engines. Deep fried sats are bad for one's career. $\endgroup$ – Deer Hunter Aug 20 '13 at 15:25
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    $\begingroup$ Space Shuttle is launched to the side, but other than that... $\endgroup$ – PearsonArtPhoto Aug 20 '13 at 15:31
  • $\begingroup$ @PearsonArtPhoto - STS' payload is in the bay, above the SSMEs :) You are clearly thinking about Buran/Energia. $\endgroup$ – Deer Hunter Aug 20 '13 at 15:36
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    $\begingroup$ On the other hand, stratospheric balloons always have the payload hanging below the balloon ;-) $\endgroup$ – gerrit Aug 20 '13 at 15:36
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    $\begingroup$ And with manned spacecraft, there is often an abort rocket atop the craft. $\endgroup$ – Deer Hunter Aug 20 '13 at 15:41
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First of all, let's look at what the limitations are for placing objects in a rocket.

  1. The object must be aerodynamic, such that it does not influence the launch characteristics.
  2. You need to easily be able to get the objects separated from the rocket.
  3. The thrust must happen at the bottom, for maximum efficacy, straight down, and the center of gravity should align with the thrust/center of drag vectors..
  4. You don't want to overheat the satellite.
  5. Every launching system to date has multiple stages.

Okay, so given all of that, what are your options, aside from a satellite launch at the top, as you mentioned? There are two things of note which I will include.

  1. The final booster could be made in to a satellite. This is rarely done, but was done with the Explorer 1, the first US satellite. The reason this is rarely done is that for the most part, the satellite and rocket are built independently, and thus, the final rocket state can't contribute to the satellite much. In addition, this still fits the satellite being the top of the stack.
  2. The Space Shuttle was launched from the side. The Space Shuttle was meant to be aerodynamic, and could take the buffeting of the ride, but it would be difficult for a non-aerodynamic object like most satellites to take the force. It lost some efficiency by its design, although it was not a significant component of loss.
  3. Abort rockets are often placed at the top of the stack for manned spaceflight missions.

The bottom line is, putting the satellite at the top is convenient to dampen vibrations, reduce aerodynamic turbulence, improve performance, reduce heating of the spacecraft, etc. It doesn't have to be done that way, but it sure makes the design a lot easier, and there aren't any compelling cases that I'm aware of to do anything differently.

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    $\begingroup$ I might add that you want the CG of the stack to be along the thrust vector when all of your engines are pointing in the same direction. If it isn't, you experience what is called "cosine losses." The shuttle, for example, experiences large cosine losses. This comes from the fact that the SSMEs (at the base of the Orbiter) must point at the CG and some of the benefit of their thrust is lost because of this. $\endgroup$ – Erik Aug 20 '13 at 17:38
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    $\begingroup$ Note that Robert Goddard's early rockets had the engine at the top, for better passive stability. $\endgroup$ – Phil Perry Jun 12 '14 at 17:59
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    $\begingroup$ Goddard thought that would make for a more stable rocket, but he was wrong. en.wikipedia.org/wiki/Pendulum_rocket_fallacy $\endgroup$ – Russell Borogove Jan 20 '15 at 0:37
  • $\begingroup$ A new comment to an old question: "The thrust must happen at the bottom". Not strictly true. The DARPA ALASA program was considering a "puller" configuration with the engines at top of the first stage. In fact the engines would be shared by first and second stage (A plumbing nightmare) $\endgroup$ – Carlos N Jun 10 '18 at 9:43
  • $\begingroup$ There are other ways it could be done, but the highest efficiency is to have the thrust at the bottom. $\endgroup$ – PearsonArtPhoto Jun 10 '18 at 9:46

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