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High-“G”-Force Impact-Landings Methods of Cargo
Delivery to the Moon, Spinning-Barrel-Style
Abstract / Pre-Summary
This
sub-page to www.rocketslinger.com is
meant to supplement the previously-published document, “High-“G”-Force Impact-Landings
Methods of Cargo Delivery to Earth’s Moon (or Other Heavenly Bodies Lacking an
Atmosphere)”. What is described here is
a lower-maintenance-costs version of the “linear decelerator” as described
there. One version described there
involved the use of “break sticks”, which would need to be replaced for every
use cycle. “Break sticks” were
envisioned as being needed to counter excessive spin-speeds that might
otherwise accumulate in the impacting cargo body, from unbalanced friction
(with the surface of the moon) on only one side of the cargo body.
Described here is
a method derived from the British spinning-barrel-bomb (AKA “bouncing bomb”) design,
which was used to destroy NAZI dams, during WW II. As our back-spinning-barrel cargo-vessel
impact-lands in a trough of moon dust (plus moon sand and gravel perhaps), the
back-spin of the vessel kicks dust (etc.) in front of it, some of which will
re-impact the spinning vessel, slowing it down.
Spin energy is killed, and traded off for deceleration energy, that is. Thus, the need for the previously-described
“break sticks” is eliminated.
Other details are
described here, such as, where, optimally, do we impart the needed spin energy
(best answer: in or on a dedicated-purpose moon-orbiting cargo-transfer
station), and how to we kill the imparted, accumulated spin energy on an
orbiting cargo-transfer station. An
answer is, use a large spinning gyroscopic mechanism,
then periodically “dump” the accumulated spin to ejected masses, such as ion
propulsion, ejected slag rock imported from the moon, or ejected space probes,
ejected by a “Spin Launch”-type device.
See https://www.spinlaunch.com/ .
As with other
sub-pages of www.rocketslinger.com , the
intent here is to “defensively publish” propulsion-related (and “misc.”) ideas,
to make them available to everyone “for free”, and to prevent “patent trolling”
of (mostly) simple, basic ideas.
Introduction
See the above abstract for the basics, some of which will
not be repeated here. See also “High-“G”-Force
Impact-Landings Methods of Cargo Delivery to Earth’s Moon (or Other Heavenly
Bodies Lacking an Atmosphere)”. This
being a rather long-winded title, it will henceforward be called the “parent
document”. See this “parent document”
Figures 4-5-6, which show a trough (or “linear
decelerator”) full of moon-dust (etc.), with Figure #6 showing the “break
sticks” that are eliminated here.
For details about the British
“bounce bomb” that we’re cribbing off of, here, see https://en.wikipedia.org/wiki/Bouncing_bomb and
https://www.sciencefocus.com/science/how-did-the-bouncing-bomb-work/ and
(best or most detailed) https://www.ukessays.com/essays/physics/physics-dambusters-bouncing-bomb-9609.php .
Enough already with the basics! Let’s get ON with it!
The Spinning-Barrel Cargo Vessel
The (sacrificial) cargo vessel should be a robustly
built, thick-walled metallic vessel.
Note that the metal shell can be molten down or otherwise re-used on the
moon. Carbon-fiber wrapping it is
another option, though. It should be
spun up to a speed approaching the maximum (beyond which it would tear itself
apart, from centrifugal force), so as to maximize spin energy that can be
traded off for deceleration. Optionally,
the vessel MIGHT be constructed to include strategically located RFID (Radio
Frequency Identity Devices) to assist in finding fragments of the vessel, if
they get buried in the moon dust of the high-G “landing strip”. Also optionally, the periphery (outer
diameter) might optimally be equipped with “saw teeth” to grip the moon dust
better, and throw it forwards, into the path of the cargo vessel.
Figure
#1
Repeated use of the “high-G-impact” landing strip will
tend to force the moon dust (plus sand and maybe gravel) “downstream”. We COULD constantly add more dust (etc.) at
one (upstream) end, and continuously lengthen the “runway” at the downstream
end. With a longer runway, we could
tweak some variables, and reduce “G” forces, thus accommodating cargo which is
less tolerant of high “G” forces, as the runway grows longer and longer over
time. Detailed math for all of this is
shown in the parent document (“G” forces v/s runway length and deceleration
time elapsed). And-or, we could
periodically collect moon dust with moon-moving machinery, pick it up at the
“downstream” end, and dump it off at the upstream end, so that it (dust, sand,
etc.) can start the journey all over again.
Or, given that the usage rate is high enough (and that we
have the money! Always, we need enough
money!), we MIGHT want to put up TWO moon-orbiting cargo-handling
“motherships”, in pro-grade v/s retrograde orbits, so as to alternately smash
the moon dust back and forth, in alternate directions! This gives us higher capital costs, yes, but also
lower maintenance costs! So it is past high
time for a topic-change new heading here…
Moon-Orbiting Cargo Motherships
The cargo vessels (from Earth for a long time to come;
from other sources eventually) COULD come directly, with “spin energy” added “en route” (along the way), but that would require wasted
(spin-adding) reaction mass. Launching
them with sufficient “spin energy” already added is a ridiculous idea, and I’m
scarcely inclined to bother to explain why.
But I’m getting ahead of myself anyway…
A cargo-handling permanently-stationed
mothership (in moon orbit) is a good idea, in this scheme! TWO of them, one orbiting pro-grade, one
orbiting retro-grade, would be even better, for reasons already explained
above. To keep them from smacking into
one another (while also keeping them both near-perfectly aligned with our
“landing strip”), we’ll want to have them assume orbits at different elevations
above the moon’s surface. Time for
another drawing…
Figure
#2
The two “cargo motherships” take in non-spinning cargo
vessels from Earth (or from other locations further in the future), add spin
energy, and then (at least in a roughly balanced manner) alternate “taking
shots on goal”, with the goals being the opposing ends of the landing strip on
the moon. By the way… substitute ice for
moon dust, in the further-distant future, if we’re shooting for the moons of
the gas giants… This should be obvious.
Well then, there’s not a whole bunch more to go
over! These cargo-handling
cargo-transfer motherships? Where
do they get their energy from, to add spin energy to the cargo vessels? Nuclear energy and solar energy sound like
good candidates to me! (Plus electrical motors, obviously!)
As they add spin energy in one direction, to the cargo
vessel, they will “want to” spin in the opposite direction, of course! We have equal and opposite actions and
reactions, always! How do we handle
that? TEMPORARILY, we cause a large
internal-to-the-mothership gyroscope to spin in the opposite direction (smaller
gyros on the two other spin axes, for a complete stability solution, also
sounds good). The “gyro” will NOT have
infinite capacity, of course!
To bleed off accumulated spin energy, we can:
‘A) Add
high-specific-impulse thrusters, such as ion propulsion, or nuclear-thermal
thrusters, or
‘B) Bring slag rock or
other low-cost materials (waste materials) from the moon, or from asteroids
(later on), for cheap reaction mass, and shoot them off in the right directions
(at the right times, so as to not hit anyone!), or
‘C) Add giant solar sails
and “tack” them the right way? I suspect
this isn’t plausible, for the scales of forces involved… Or
‘D) (My favorite choice!)
add a “Spin Launch”-type device (see https://www.spinlaunch.com/ ) to
shoot off planetary and-or interstellar probes, when the right opportunities
present themselves! This may not be
often… So this method would likely need
to be combined with other methods.
Other clever combinations and variations of the above
will likely make sense. Choice “B”
variations might include solidifying your waste materials to be shot off, so
that one can SPIN the material (for spin-energy-dumping of course), as well as
get reaction mass out of it. If
solidifying it (to withstand high spin energy) is expensive or impractical, we
could even get “Rube Goldberg-esque” here, and devise
a large shotgun-style device, where the shotgun-cartridge segment of the barrel
(if not the entire barrel) is rotated at high speeds, before the slag or other
waste is “shot off”. Sounds like Wyle
Coyote designed it, yes! But it COULD
work, and be more efficient at spin-energy-dumping!
I have
no special expertise or any more plausible ideas concerning any associated
matters here, so I will sign off at this time.
This concludes my ideas as of this time.
Once again, comments or questions (or idea contributions) are welcomed
at RocketSlinger@SBCGlobal.net …
Stay tuned… Talk to me!
RocketSlinger@SBCGlobal.net
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References
Stauffer,
Titus. (2020). High-“G”-Force Impact-Landings
Methods of Cargo Delivery to Earth’s Moon (or Other Heavenly Bodies Lacking an
Atmosphere)