Is laser space propulsion practical?: review
[PHYS]Physics [physics]
[SPI]Engineering Sciences [physics]
[SDU]Sciences of the Universe [physics]
13. Climate action
[SDE]Environmental Sciences
0103 physical sciences
7. Clean energy
01 natural sciences
DOI:
10.1364/ao.434245
Publication Date:
2021-09-07T20:30:05Z
AUTHORS (6)
ABSTRACT
In this paper, we review practical limitations to laser space
propulsion that have been discussed in the literature. These are as
follows: (1) thermal coupling to the propelled payload, which might
melt it; (2) a decrease in mechanical coupling with number of pulses,
which has been observed in some cases; and (3) destruction of solar
panels in debris removal proposals that might create more debris
rather than less. Previously, lack of data prevented definite
assessments. Now, new data on multipulse vacuum laser impulse coupling
coefficient
C
m
on several materials at 1064 nm, at
1030 nm, and at 532 nm are available. We are now able to compare the
results for single and multiple pulses on materials that have been
considered for laser ablation space propulsion (LASP), or that are
likely space debris constituents, and decide whether LASP is a
practical idea. Laser space propulsion and debris removal concepts
depend on thousands or hundreds of thousands of repetitive pulses.
Repetitive pulse mechanical coupling as well as thermal coupling
(which can melt the target rather than propel it) are both important
considerations. Materials studied were 6061T6 aluminum, carbon-doped
polyoxymethylene (POM), undoped POM, a yellow POM copolymer, and a
mixture of Al and POM microparticles combined and pressed, containing
a 50%/50% mixture of the two materials by mass. We address 6 and 70 ps
pulses because of the availability of data at these pulse durations.
We also briefly consider continuous wave (CW) laser propulsion.
Finally, we consider a recent paper concerning solar panel destruction
from a positive perspective.
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