ATTITUDE CONTROL SYSTEM OF THE SOUNDING ROCKET S-520-5.

Ichiro Nakatani, Jun ichiro Kawaguchi, Toshiya Nakajima, Ritsuo Hasegawa

Research output: Contribution to conferencePaperpeer-review

1 Citation (Scopus)
Original languageEnglish
Pages981-986
Number of pages6
Publication statusPublished - 1982
Externally publishedYes

ASJC Scopus subject areas

  • Engineering(all)

Cite this