TY - JOUR
T1 - Analysis of laser wavelength and energy dependences of the impulse in a magnetic thrust chamber system for a laser fusion rocket
AU - Maeno, Akihiro
AU - Yamamoto, Naoji
AU - Fujioka, Shinsuke
AU - Mori, Yoshitaka
AU - Sunahara, Atsushi
AU - Johzaki, Tomoyuki
AU - Nakashima, Hideki
PY - 2013/5
Y1 - 2013/5
N2 - Experiments using a pendulum thrust stand are performed to determine the dependences of the impulse on the laser wavelength and energy in a magnetic thrust chamber system for a laser fusion rocket. The impulse is generated by the interaction between a diamagnetic current in a laser-produced plasma and a magnetic field. The plasma is produced by irradiating a spherical polyacetal target with a single-beam glass laser (laser pulse duration: 1.3 ns; laser wavelengths: 1,053, 527 and 351 nm; laser energy: 30-900 J). The magnetic field is generated by a cylindrical neodymium permanent magnet (50mm diameter and 40mm long) placed in a position 33mm from the target. Impulses in the range 0.02- 10 mNs are measured using a pendulum thrust stand. The experiments reveal that the impulse for 2ω is similar to that for 3ω, and is larger than that for ω.
AB - Experiments using a pendulum thrust stand are performed to determine the dependences of the impulse on the laser wavelength and energy in a magnetic thrust chamber system for a laser fusion rocket. The impulse is generated by the interaction between a diamagnetic current in a laser-produced plasma and a magnetic field. The plasma is produced by irradiating a spherical polyacetal target with a single-beam glass laser (laser pulse duration: 1.3 ns; laser wavelengths: 1,053, 527 and 351 nm; laser energy: 30-900 J). The magnetic field is generated by a cylindrical neodymium permanent magnet (50mm diameter and 40mm long) placed in a position 33mm from the target. Impulses in the range 0.02- 10 mNs are measured using a pendulum thrust stand. The experiments reveal that the impulse for 2ω is similar to that for 3ω, and is larger than that for ω.
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U2 - 10.2322/tjsass.56.170
DO - 10.2322/tjsass.56.170
M3 - Article
AN - SCOPUS:84878189472
SN - 0549-3811
VL - 56
SP - 170
EP - 172
JO - Transactions of the Japan Society for Aeronautical and Space Sciences
JF - Transactions of the Japan Society for Aeronautical and Space Sciences
IS - 3
ER -