FIELD: aircraft engineering.
SUBSTANCE: proposed module comprises bearing housing composed of grate-cylindrical shells with ends coupled with semispherical shells. Top semispherical shell housing has through holes to receive ionising transducer sensors, shell outer surface being coated with sandwiched coat of alternating layers of polarised material of piezo-active film and aero gel. Sandwiched coating is applied to bottom semispherical shell outer side to make capacitor-type transducer. Through hole is made at crossing between onboard module lengthwise axis with housing of bottom hemispherical shell housing for connection of hollow adapter for installation of onboard module at spaceship body and protection of electric communication. Said module is equipped with aero gel traps arranged in detachable exposed flasks. Said flasks are arranged in all cells at grate-cylindrical shell in several parallel rows, mat least in four row spaced apart through 90 degrees. Sandwiched PVDF-aero gel detectors are fitted in said flasks as well as cellular and rectangular sets of aero gel traps are arranged in said flasks. All aforesaid are made from UV-radiation-resistant material.
EFFECT: increased data content of measurement procedures.
5 cl, 3 dwg
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Authors
Dates
2014-01-27—Published
2012-06-22—Filed