Some subsystems of payload S29

Details Some subsystems of payload S29 Some subsystems of payload S29

Jun 1978

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1978esasp.135..441a&link_type=abstract

In ESA European Sounding Rocket, Balloon and Related Res., with Emphasis on Expt. at High Latitudes p 441-447 (SEE N79-31637 2

Computer Science

Sound

Nike Rocket Vehicles, Payloads, Rocket Nose Cones, Sounding Rockets, Apogees, Booms (Equipment), Magnetometers, Rocket Launching, Sweden, Yo-Yo Devices

Scientific paper

The S29 sounding rocket is described. A launch from Esrange is planned for March or April 1979. The payload has a total weight of 193 kg and will be launched to an apogee altitude of 405 km with a Nike-Black Brant VC rocket. Some technically interesting subsystems are described including: a split nose cone, radially and forward deployable booms, which are cheap and simple, yet permit repeated testing, a yoyo device to introduce deliberate coning automatically released at the desired roll angle using magnetometer signals, and a mechanism for forward separation on ground command, of a Barium shaped charge.

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