Physics
Scientific paper
Jun 1980
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1980esasp.152..155w&link_type=abstract
In ESA European Rocket and Balloon Programs and Related Res. p 155-160 (SEE N81-10914 01-99)
Physics
Helium, Payloads, Rocket-Borne Instruments, Ultraviolet Spectrophotometers, Apogees, Attitude Control, Skylark Rocket Vehicle, Three Axis Stabilization
Scientific paper
A technical description of a three axes stabilized payload developed for the three stage rocket Skylark 12 and designed for an apogee of more than 800 km is given. The scientific payload is a helium resonance cell EUV photometer instrumented for high resolution spectral analysis of He I 58.4 nm and He II 30.4 nm radiation. The experiment which consists mainly of four measuring cells, supply systems, and baffle system, is accommodated in the top payload section and covered by a split nose cone during ascent.
Henkel R.
Weber Richard R.
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