Attitudes of the Antarctic Sounding Rocket Vehicles

P(論文) The attitudes of the 12 sounding rockets which were launched at Syowa Station in Antarctica from May 1972 to August 1973 were determined by geomagnetic aspect sensors. The attitudes of the latest launched sounding rockets, S-210JA-22 and S-310JA-1 were also determinated. The three-dimensional...

Full description

Bibliographic Details
Main Authors: Tohyama, Fumio, Aoyama, Iwao
Language:English
Published: 1978
Subjects:
Online Access:https://nipr.repo.nii.ac.jp/record/910/files/KJ00000011883.pdf
id ftnipr:oai:nipr.repo.nii.ac.jp:00000910
record_format openpolar
spelling ftnipr:oai:nipr.repo.nii.ac.jp:00000910 2024-09-09T19:04:03+00:00 Attitudes of the Antarctic Sounding Rocket Vehicles Tohyama, Fumio Aoyama, Iwao 1978-10 application/pdf https://nipr.repo.nii.ac.jp/record/910/files/KJ00000011883.pdf eng eng Memoirs of National Institute of Polar Research. Special issue 9 87 91 AA00733561 https://nipr.repo.nii.ac.jp/record/910/files/KJ00000011883.pdf 1978 ftnipr 2024-06-17T04:04:30Z P(論文) The attitudes of the 12 sounding rockets which were launched at Syowa Station in Antarctica from May 1972 to August 1973 were determined by geomagnetic aspect sensors. The attitudes of the latest launched sounding rockets, S-210JA-22 and S-310JA-1 were also determinated. The three-dimensional orientation of the S-210JA-22 rocket axis was obtained by the geomagnetic aspect sensors and the solar aspect sensor. The result shows that the precessional motion of the S-210JA-22 vehicle included the geomagnetic field line. The spin frequency of these 14 vehicles was mostly in the range from 1.1 to 1.3Hz and their conical (precessional) half angle was mostly from 20 to 60 degrees, with the conical rotational period mostly from 50 to 120 seconds. departmental bulletin paper Other/Unknown Material Antarc* Antarctic Antarctica Memoirs of National Institute of Polar Research Polar Research National Institute of Polar Research Repository, Japan Antarctic Syowa Station The Antarctic
institution Open Polar
collection National Institute of Polar Research Repository, Japan
op_collection_id ftnipr
language English
description P(論文) The attitudes of the 12 sounding rockets which were launched at Syowa Station in Antarctica from May 1972 to August 1973 were determined by geomagnetic aspect sensors. The attitudes of the latest launched sounding rockets, S-210JA-22 and S-310JA-1 were also determinated. The three-dimensional orientation of the S-210JA-22 rocket axis was obtained by the geomagnetic aspect sensors and the solar aspect sensor. The result shows that the precessional motion of the S-210JA-22 vehicle included the geomagnetic field line. The spin frequency of these 14 vehicles was mostly in the range from 1.1 to 1.3Hz and their conical (precessional) half angle was mostly from 20 to 60 degrees, with the conical rotational period mostly from 50 to 120 seconds. departmental bulletin paper
author Tohyama, Fumio
Aoyama, Iwao
spellingShingle Tohyama, Fumio
Aoyama, Iwao
Attitudes of the Antarctic Sounding Rocket Vehicles
author_facet Tohyama, Fumio
Aoyama, Iwao
author_sort Tohyama, Fumio
title Attitudes of the Antarctic Sounding Rocket Vehicles
title_short Attitudes of the Antarctic Sounding Rocket Vehicles
title_full Attitudes of the Antarctic Sounding Rocket Vehicles
title_fullStr Attitudes of the Antarctic Sounding Rocket Vehicles
title_full_unstemmed Attitudes of the Antarctic Sounding Rocket Vehicles
title_sort attitudes of the antarctic sounding rocket vehicles
publishDate 1978
url https://nipr.repo.nii.ac.jp/record/910/files/KJ00000011883.pdf
geographic Antarctic
Syowa Station
The Antarctic
geographic_facet Antarctic
Syowa Station
The Antarctic
genre Antarc*
Antarctic
Antarctica
Memoirs of National Institute of Polar Research
Polar Research
genre_facet Antarc*
Antarctic
Antarctica
Memoirs of National Institute of Polar Research
Polar Research
op_relation Memoirs of National Institute of Polar Research. Special issue
9
87
91
AA00733561
https://nipr.repo.nii.ac.jp/record/910/files/KJ00000011883.pdf
_version_ 1809818049281261568