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<strong>The</strong> Ultimate Limits of the Relativistic <strong>Rocket</strong> Equation<br />

<strong>The</strong> <strong>Planck</strong> <strong>Photon</strong> <strong>Rocket</strong><br />

Espen Gaarder Haug ⇤<br />

Norwegian University of Life Sciences<br />

January 11, 2017<br />

UNARMED SERVICES TECHNICAL INFORMATION AGENCY: This information must not be distributed<br />

or leaked to hostile extraterrestrial life or organizations supporting these. If this information is leaked, then<br />

hostile aliens could be here before we know it! People, entities, and leak-organizations even suspected for<br />

misconduct will be prosecuted and potentially used as rocket fuel! For unclassified documentations see<br />

<br />

Abstract<br />

In this paper we look at the ultimate limits of a photon propulsion rocket. <strong>The</strong> maximum velocity<br />

for a photon propulsion rocket is just below the speed of light and is a function of the reduced Compton<br />

wavelength of the heaviest subatomic particles in the rocket. We are basically combining the relativistic<br />

rocket equation with Haug’s new insight on the maximum velocity for anything with rest mass; see [1, 2, 3].<br />

An interesting new finding is that in order to accelerate any subatomic “fundamental” particle to its<br />

maximum velocity, the particle rocket basically needs two <strong>Planck</strong> masses of initial load. This might sound<br />

illogical until one understands that subatomic particles with di↵erent masses have di↵erent maximum<br />

velocities. This can be generalized to large rockets and gives us the maximum theoretical velocity of a<br />

fully-e cient and ideal rocket. Further, no additional fuel is needed to accelerate a <strong>Planck</strong> mass particle<br />

to its maximum velocity; this also might sound absurd, but it has a very simple and logical solution that<br />

is explained in this paper.<br />

Key words: Relativistic rocket equation, photon propulsion, rocket load, maximum speed rocket,<br />

<strong>Planck</strong> mass, <strong>Planck</strong> length, reduced Compton wavelength, electron.<br />

1 Introduction<br />

Haug [3] has recently introduced a new maximum velocity for subatomic particles (anything with mass)<br />

that is just below the speed of light given by<br />

v max = c<br />

r<br />

where ¯ is the reduced Compton wavelength of the particle we are trying to accelerate and l p is the<br />

<strong>Planck</strong> length, [4]. This maximum velocity puts an upper boundary condition on the kinetic energy, the<br />

momentum, and the relativistic mass, as well as on the relativistic Doppler shift in relation to subatomic<br />

⇤ e-mail espenhaug@mac.com. Thanks to Victoria Terces for helping me edit this manuscript. Also thanks to Alan Lewis,<br />

Daniel Du↵y, ppauper and AvT for useful tips on how to do high precision calculations.<br />

1<br />

l 2 p<br />

¯2<br />

(1)<br />

1


2<br />

particles. Basically, no fundamental particle can attain a relativistic mass higher than the <strong>Planck</strong> mass,<br />

and the shortest reduced Compton wavelength we can observe from length contraction is the <strong>Planck</strong><br />

length. In addition, the maximum frequency is limited to the <strong>Planck</strong> frequency, the <strong>Planck</strong> particle mass<br />

is invariant, and so is the <strong>Planck</strong> length (when related to the reduced Compton wavelength).<br />

Here we will combine this equation with the relativistic rocket equation in order to assess how much<br />

fuel would be needed to accelerate an ideal particle rocket to its maximum velocity. We will also extend<br />

this concept to look at the ultimate velocity limit for a macroscopic rocket traveling under ideal conditions<br />

(in a vacuum).<br />

2 <strong>The</strong> Limits of the <strong>Photon</strong> <strong>Rocket</strong><br />

<strong>The</strong> Ackeret [5] relativistic rocket equation is given by 1<br />

and solved with respect to velocity we have<br />

1+ v<br />

c<br />

m 0 = m 1<br />

1<br />

v<br />

c<br />

! c<br />

2Isp<br />

✓ ✓ ◆◆<br />

Isp<br />

v = c tanh<br />

c ln mo<br />

m 1<br />

(2)<br />

(3)<br />

where I SP is the specific impulse, which is a measure of the e ciency of a “rocket”, m 1 is the final rest<br />

mass of the rocket (payload), and m 0 is the initial rest mass of the rocket (payload plus fuel). We will<br />

assume that the internal e ciency of the rocket drive is 100 percent, that is I SP<br />

c<br />

=1. Thisisbasically<br />

equivalent to a rocket driven by photon propulsion, or a so-called photon rocket, see [11, 12, 13]. Next we<br />

are interested in estimating the amount of fuel needed to accelerate a subatomic particle (using a photon<br />

propulsion particle engine) to the Haug maximum velocity, and we get<br />

1+ vmax<br />

c<br />

m 0 = m 1 v<br />

1 max<br />

c<br />

0 r<br />

m 0 = m 1<br />

B<br />

1+ c 1<br />

r<br />

@<br />

c 1<br />

1<br />

0 q<br />

m 0 = m 1<br />

@ 1+ 1<br />

q<br />

1 1<br />

l 2 p<br />

¯2<br />

c<br />

l 2 p<br />

¯2<br />

c<br />

! 1<br />

2<br />

l 2 p<br />

¯2<br />

l 2 p<br />

¯2<br />

1<br />

C<br />

A<br />

1<br />

2<br />

1<br />

A<br />

1<br />

2<br />

(4)<br />

when ¯ >>l<br />

q p, as is the case for any observed fundamental particle, we can approximate with a series<br />

l<br />

expansion: 1<br />

2 p<br />

1 l<br />

¯2 ⇡ 1<br />

2 p<br />

2 ¯2 , and we get<br />

0<br />

1<br />

m 0 ⇡ m 1<br />

@ 1+1 1 l 2 p<br />

2 ¯2<br />

A<br />

1 1+ 1 l 2 p<br />

2 ¯2<br />

0 1<br />

m 0 ⇡ m 1<br />

@ 2 1 l 2 1<br />

2<br />

p<br />

2 ¯2<br />

A<br />

0<br />

m 0 ⇡ m 1<br />

@ 4<br />

1 l 2 p<br />

2 ¯2<br />

l 2 p<br />

¯2<br />

l 2 p<br />

¯2<br />

1<br />

A<br />

1<br />

2<br />

1<br />

2<br />

(5)<br />

Since we assume that ¯ >>l p, then this can be further approximated quite well by<br />

1 See also [6], [7], [8], [9] and[10].


3<br />

m 0 ⇡<br />

s<br />

4<br />

m 1<br />

l 2 p<br />

¯2<br />

2¯<br />

m 0 ⇡ m 1 =2m p<br />

l p<br />

(6)<br />

This means that in order to accelerate any particle (an electron, for example) to its maximum velocity<br />

we need a particle rocket with two <strong>Planck</strong> masses of fuel, 2m p ⇡ 4.35302 ⇥ 10 08 kg. <strong>The</strong> velocity of the<br />

electron will then be<br />

✓ ✓ ◆◆ 2mp<br />

v max = c tanh ln<br />

m e<br />

= c<br />

⇣ ⌘ 2 2mp<br />

m e<br />

1<br />

⇣ ⌘ 2<br />

⇡ c⇥0.999999999999999999999999999999999999999999999124<br />

2mp<br />

m e<br />

+1<br />

(7)<br />

<strong>The</strong> Einstein relativistic mass 2 of the electron is then equal to the <strong>Planck</strong> mass. This is the same<br />

maximum velocity as given by [1, 2]. <strong>The</strong>se calculations require very high precision and were calculated<br />

in Mathematica. 3<br />

Remarkably, the concept of two <strong>Planck</strong> masses being used as fuel to reach the maximum velocity for<br />

a subatomic particle holds for any particle. Naturally, this can only work because the maximum velocity<br />

of heavier particles is lower than that of lighter particles.<br />

<strong>The</strong> equation 6 above is only a good approximation as long as ¯ >>l p, which is the case for all<br />

observed subatomic particles so far. In the special case, we initially have a payload equal to the <strong>Planck</strong><br />

mass particle with m 1 = m p we must have ¯ = l p, so we need to use the equation as it was before we<br />

applied the series approximation expansion<br />

0 q<br />

m 0 = m 1<br />

@ 1+ 1<br />

q<br />

1 1<br />

0 r<br />

1+ 1<br />

m 0 = m p<br />

B<br />

@<br />

r<br />

1 1<br />

l 2 p<br />

¯2<br />

l 2 p<br />

¯2<br />

l 2 p<br />

l 2 p<br />

l 2 p<br />

l 2 p<br />

1<br />

A<br />

1<br />

C<br />

A<br />

1<br />

2<br />

1<br />

2<br />

m 0 = m p<br />

✓ 1<br />

1<br />

◆ 1<br />

2<br />

= mp (8)<br />

In other words, as we accelerate the <strong>Planck</strong> mass particle to its maximum velocity we will need no<br />

extra mass as fuel. At first this may seem absurd, as we will always need some energy for the acceleration.<br />

However, the solution is simple; as [1] has shown, the <strong>Planck</strong> mass particle must always be at rest when<br />

observed from any reference frame, the <strong>Planck</strong> mass particle and the <strong>Planck</strong> length are remarkably<br />

invariant entities. <strong>The</strong> maximum velocity of a <strong>Planck</strong> mass particle is<br />

r s<br />

lp<br />

v max = c 1<br />

2 = c lp<br />

1<br />

2 =0 (9)<br />

¯2<br />

<strong>The</strong> <strong>Planck</strong> mass particle is the very turning point of light. What is the velocity of light at the precise<br />

instant when it changes direction? According to Haug, at this very instant it will be at rest. In the very<br />

next instant, the <strong>Planck</strong> particle will be dissolved into energy.<br />

3 Relation to the Tipler Factor of 2<br />

It is also worth noting that our result of two <strong>Planck</strong> masses as the initial q mass needed to accelerate a<br />

payload for any 4 l<br />

fundamental particle to its maximum velocity, v max = c 1<br />

2 p<br />

¯2 ,seemstobeconsistent<br />

2 See [14] and[1].<br />

We used several di↵erent set-ups in Mathematica; here is one of them: N[Sqrt[1 (1616199 ⇤ 10^( 41))^2/(3861593 ⇤ 10^( 19))^2], 50],<br />

where 1616199 ⇤ 10^( 41) is the <strong>Planck</strong> length and 3861593 ⇤ 10^( 19) is the reduced Compton wavelength of the electron.<br />

An alternative way to write it is: N[Sqrt[1 (SetPrecision[1.616199 ⇤ 10^( 35))^2, 50]/(SetPrecision[3.861593 ⇤ 10^( 13))^2, 50]], 50].<br />

4 Except the <strong>Planck</strong> mass particle itself.<br />

l 2 p


4<br />

with an interesting result presented by Tipler in 1999, see [16]. Tipler discussed what he called “ultrarelativisitic<br />

rockets,” these are rockets basically moving at a speed very close to that of light. Tipler has<br />

shown that for a photon rocket, the total initial mass-energy that is needed to accelerate the payload to<br />

a velocity very close to that of light only is twice the payload energy-mass as measured from the Earth<br />

(the relativistic mass of the payload when the payload has reached its final velocity, very close to the<br />

speed of light). <strong>The</strong> initial mass is still enormous compared to the rest-mass of the payload, but is only 2<br />

in relation to the final relativistic payload mass. We also get the same result from the maximum velocity<br />

formula and analysis above. <strong>The</strong> relativistic mass of any fundamental particle traveling at its maximum<br />

velocity is<br />

q<br />

c 1<br />

m 1<br />

=<br />

vmax<br />

2<br />

c 2<br />

c<br />

s<br />

1<br />

m 1<br />

l<br />

r<br />

l 2 ! 2<br />

= m 1<br />

p¯<br />

p<br />

c 1 ¯2<br />

c 2<br />

= mp (10)<br />

and we find that to accelerate any particle (payload) to this velocity we need two <strong>Planck</strong> masses of<br />

initial mass (energy). In more general terms, we can write this as<br />

r<br />

1<br />

m 0<br />

m 1<br />

v2 max<br />

c 2<br />

= 2mp<br />

m 1<br />

l p¯<br />

=<br />

2m p<br />

v<br />

m 1<br />

0 s<br />

l 2 12<br />

p<br />

u @c 1 A<br />

t ¯2<br />

c 1<br />

c 2<br />

= 2mp<br />

m 1<br />

l p¯<br />

=2 (11)<br />

Our result can be seen as the subatomic derivation/connection to the same result as given by Tipler.<br />

However, our result derived for subatomic particles seems to provide additional insight. According to our<br />

theory, the Tipler result of factor 2 is also valid at rocket velocities considerably below c, ifthesubatomic<br />

fundamental particles accelerated are super heavy, that is significant relative to the <strong>Planck</strong> mass 5 . And<br />

again in the special case of a <strong>Planck</strong> mass we actually have a maximum velocity of zero and no additional<br />

fuel is needed to accelerate the object that is at rest. Yet, this can only hold true if the <strong>Planck</strong> mass<br />

particle only lasts for an instant.<br />

4 Maximum Velocity of <strong>Rocket</strong> Ship<br />

<strong>The</strong> maximum velocity of any composite object (even a nucleus) is likely to be limited by the fundamental<br />

particle with the shortest reduced Compton wavelength from which it is constructed. In other words, the<br />

speed limit of a rocket is limited by the heaviest subatomic “fundamental” particle it is built from. When<br />

this particle reaches its maximum velocity, that is given by<br />

v max = c<br />

r<br />

it will first turn into a <strong>Planck</strong> mass particle and then will burst into energy. If this type of fundamental<br />

particle is a significant part of the macroscopic object (spaceship) we are traveling in, then the whole ship<br />

is likely to be destroyed at the moment we reach this velocity. If the proton was a fundamental particle,<br />

then the maximum velocity of a rocket traveling under ideal conditions (in a vacuum) would be 6<br />

v = c<br />

s<br />

1<br />

1<br />

l 2 p<br />

¯2<br />

(12)<br />

l 2 p<br />

¯2<br />

P<br />

= c ⇥ 0.99999999999999999999999999999999999999705 (13)<br />

For comparison, at the Large Hadron Collider in 2008, the team talked about the possibility of<br />

accelerating protons to the speed of 99.9999991% of the speed of light [15]. When the Large Hadron<br />

Collider went full force in 2015, they increased the maximum speed slightly above this (likely to around<br />

99.99999974% of the speed of light). In reality, if a proton consists of a series of other subatomic particles,<br />

then the speed limit given above for a proton will not be very accurate. Alternatively, we could have<br />

looked at the reduced Compton wavelength of the quarks that the standard model claims make up the<br />

proton.<br />

5 <strong>The</strong> Ultimate Limitations on Nano-scale Bullets<br />

<strong>The</strong> analysis above also gives some ultimate limitations on small weaponry. One could think of the<br />

limitation on an electron rocket gun, for example. Electrons accelerated to their maximum velocity<br />

5 In other words for subatomic particles with much shorter reduced Compton wavelength than the ones observed so far.<br />

6 Here assuming l p =1.616199 ⇥ 10 35 and ¯P =2.10309 ⇥ 10 16 .


5<br />

would have enormous kinetic energy compared to today’s primitive small arms, but even so, they would<br />

have less kinetic energy than one might expect, based on the content in certain physics textbooks that<br />

give no limits on how close v can get to c, see[17]. <strong>The</strong> kinetic energy from a single bullet would be<br />

approximately<br />

k e =<br />

q<br />

1<br />

m e<br />

v 2 max<br />

c 2<br />

✓ ◆<br />

m ec 2 1 1<br />

=¯hc<br />

⇡ m pc 2 ⇡ 1, 956, 149, 410 Joule,<br />

l p<br />

¯e<br />

while (for example) the kinetic energy from a 44 magnum revolver with a 240-grain (16 g) bullet<br />

traveling at 500 m/s is only k e,44m ⇡ 1 2 0.016 ⇥ 5002 =2, 000 Joule. This means that the photon rocket<br />

gun has about 978,075 times more impact energy than a 44 magnum; that is an enormous di↵erence. One<br />

of the additional benefits of such a gun is the massive quantity of bullets it could carry, each bullet having<br />

a rest mass of only 2m p ⇡ 0.000044g. (When someone comes with a 44 magnum, show them your <strong>Planck</strong><br />

0.000044 magnum gun and tell them size does not necessarily matter!). One could potentially think of<br />

each bullet as one <strong>Planck</strong> mass of matter and one <strong>Planck</strong> mass of antimatter (plus an electron?). When<br />

the antimatter and matter <strong>Planck</strong> mass are united, this could convert the fuel into acceleration photon<br />

energy (photon rocket fuel), at least hypothetically.<br />

Such a rocket-gun would likely never run out of bullets, a 50-gram magazine would give 1,148,628<br />

bullets. Of course, one would need containers for the fuel and so forth. Hopefully such a gun will never<br />

come into existence, but as with many new inventions (and equations), the emerging capabilities can be<br />

used for good and for bad. If such advanced technology were built into our i-Phones, for example, it<br />

could potentially be used as an energy generator to provide heat and electricity for an entire house for<br />

months, if not years. And in case of an alien invasion, one would be happy to have a seemingly innocent<br />

energy-generating device that could convert itself into a very powerful gun.<br />

6 Summary and Conclusion<br />

<strong>The</strong> maximum amount of fuel needed for any fully-e cient particle rocket is equal to two <strong>Planck</strong> masses.<br />

This amount of fuel will bring any subatomic particle up to its maximum velocity. At this maximum<br />

velocity the subatomic particle will itself turn into a <strong>Planck</strong> mass particle and likely will explode into<br />

energy. Interestingly, we need no fuel to accelerate a fundamental particle that has a rest-mass equal to<br />

<strong>Planck</strong> mass up to its maximum velocity. This is because the maximum velocity of a <strong>Planck</strong> mass particle<br />

is zero as observed from any reference frame. However, the <strong>Planck</strong> mass particle can only be at rest for<br />

an instant. <strong>The</strong> <strong>Planck</strong> mass particle can be seen as the very turning point of two light particles; it exists<br />

when two light particles collide 7 . Haug’s newly-introduced maximum mass velocity equation seems to be<br />

fully consistent with application to the relativistic rocket equation and it gives an important new insight<br />

into the ultimate limit of fully-e cient particle rockets.<br />

7 See [1] foradetaileddiscussionandpresentationofanatomismparticlemodel.


6<br />

Appendix<br />

This shows a slightly di↵erent and slightly more complex way to derive the same result. In the case of a<br />

photon rocket, when combined with Haug’s maximum velocity for subatomic particles, we have<br />

✓<br />

artanh<br />

✓ ✓<br />

mo<br />

v max = c tanh ln<br />

v max<br />

c<br />

vmax<br />

c<br />

◆<br />

✓<br />

= tanh ln<br />

✓ ◆<br />

mo<br />

= ln<br />

m 1<br />

vmax<br />

e<br />

artanh(<br />

c ) = mo<br />

m 1<br />

m 0 = m 1e<br />

m 0 = m 1e<br />

◆◆<br />

m 1<br />

✓ ◆◆<br />

mo<br />

m 1<br />

vmax<br />

artanh(<br />

c )<br />

0 s<br />

l 2 1<br />

p<br />

c 1<br />

artanhB<br />

¯2<br />

C<br />

@ c A<br />

m 0 = m 1e artanh r<br />

m 0 = m 1e<br />

Further, when ¯ >>l p we can use a series approximation,<br />

m 0 ⇡ m 1e<br />

m 0 ⇡ m 1e<br />

0<br />

m 0 ⇡ m 1<br />

@ 2 1<br />

2<br />

m 0 ⇡ m 1<br />

v uuut<br />

4<br />

1<br />

0 s<br />

1<br />

2 ln 1+ 1<br />

B s<br />

@<br />

1 1<br />

q<br />

1<br />

0<br />

1<br />

2 ln 1+1 1 l 2 1<br />

p<br />

B 2 ¯2<br />

@<br />

1 1+ 1 l 2 C<br />

A<br />

p<br />

2 ¯2<br />

0<br />

1<br />

2 ln 2 1 l 2 1<br />

p<br />

B 2 ¯2<br />

@ l<br />

1<br />

2 C<br />

A<br />

p<br />

2 ¯2<br />

1 l 2 p<br />

2 ¯2<br />

l 2 p<br />

¯2<br />

1<br />

A<br />

1<br />

2<br />

l 2 !<br />

p<br />

¯2<br />

l 2 p<br />

¯2<br />

l 2 p<br />

¯2<br />

1<br />

C<br />

A<br />

l 2 p<br />

¯2 ⇡ 1<br />

Further, when ¯ >>l p, then then this can be very well-approximated by<br />

l 2 p<br />

¯2<br />

l 2 p<br />

¯2<br />

1 l 2 p<br />

2 ¯2 ,thisgives<br />

(14)<br />

(15)<br />

m 0 ⇡<br />

s<br />

4<br />

m 1<br />

l 2 p<br />

¯2<br />

2¯<br />

m 0 ⇡ m 1 =2m p<br />

l p<br />

(16)<br />

This is the same result as we obtained in the main part of the paper using a slightly easier derivation.


7<br />

References<br />

[1] E. G. Haug. <strong>The</strong> <strong>Planck</strong> mass particle finally discovered! Good bye to the point particle hypothesis!<br />

http://vixra.org/abs/1607.0496, 2016.<br />

[2] E. G. Haug. A new solution to Einstein’s relativistic mass challenge based on maximum frequency.<br />

http://vixra.org/abs/1609.0083, 2016.<br />

[3] E. G. Haug. <strong>The</strong> gravitational constant and the <strong>Planck</strong> units. A simplification of the quantum realm.<br />

Physics Essays Vol 29, No 4, 2016.<br />

[4] M. <strong>Planck</strong>. <strong>The</strong> <strong>The</strong>ory of Radiation. Dover 1959 translation, 1906.<br />

[5] J. Ackeret. Zur theorie der racketen. Helvetica Physica Acta, 19:103–2509,1946.<br />

[6] W. L. Bade. Relativistic rocket theory. American Journal of Physics, 310(21),1953.<br />

[7] K. B. Pomeranz. <strong>The</strong> relativistic rocket. American Journal of Physics, 565(34),1966.<br />

[8] G. Vulpetti. Maximum terminal velocity of relativistic rocket. Acta Astronautica, 85(2):81–90,1985.<br />

[9] U. Walter. Relativistic rocket and space flight. Acta Astronautica, 59(6),2006.<br />

[10] A. F. Antippa. <strong>The</strong> relativistic rocket. European Journal of Physics, 30:605–613,2009.<br />

[11] G. G. Zelkin. A photon rocket. Priroda (Nature), 11:1–9,1960.<br />

[12] V. Snilga. <strong>The</strong>re will be no photon rocket. Bulletin of the Astronomical Institute of Czechoslovakia,<br />

7:31–33, 1960.<br />

[13] P. Burcev. On the mechanics of photon rockets. Bulletin of the Astronomical Institute of Czechoslovakia,<br />

15:79–81,1964.<br />

[14] A. Einstein. Zur elektrodynamik bewegter körper. Annalen der Physik, (17),1905.<br />

[15] G. Brumfiel. LHC by the numbers. News: Briefing, Nature, Published online 9 September, 2008.<br />

[16] F. Tipler. Ultrarelativistic rockets and the ultimate future of the ultimate future of the universe.<br />

NASA Breakthrough Propulsion Physics Workshop Proceedings, 1999.<br />

[17] E. G. Haug. Modern physics’ incomplete absurd relativistic mass interpretation. and the simple<br />

solution that saves Einstein’s formula. http://vixra.org/abs/1612.0249, 2016.

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