Purpose of the flight and payload description
The fast neutron detector was an instrument aimed to measure 1-10 Mev recoil-proton and heavily ionizing events produced by neutrons in an organic scintillator. The detector itself is a 5 cm x 5 cm cylindrical volume of organic liquid phosphor, which is surrounded by a 6 mm minimum thickness of plastic scintillator which acts as an anticoincidence shield for charged particles. The composite detector is viewed by a single 5 cm photomultiplier. The set is shown in the far left scheme.
Events produced in the composite scintilator by radiation other than neutrons (like protons and electrons produced by background radiation and gamma rays) are rejected by the detector electronics on the basis of pulse shape. The pulses produced by scintillations of recoil-protons between 1 and 10 MeV are amplified, gated as neutron events and sorted in a seven-channel pulse height analyzer. The seven channels of pulse height information are binary coded and recorded on three tracks of a four track magnetic tape recorder. The fourth track contains a time signal as well as a record of all events produced in the scintillator with a light output greater than that of 1 MeV proton. Ambient pressure, the temperature of the gondola, and time are registered by a photobarograph which also acts as a backup system for the tape recorder, registering the counts in neutron channels 1-5 and 4-7 and in total events.
The instrumented rack (shown in the far right scheme) was designed so that the mass distributed in the balloon gondola would subtend a minimal solid angle at the scintillator. This was to prevent background neutrons produced by high energy radiation in the local material, from reaching the detector. An exterior container housed the photobarograph and the batteries for the heaters in the gondola. Such heaters were required only during night flights, since the insulation, made of 10 cm of polyurethane foam, and the reflectivity of the yellow fiberglas gondola were sufficient to maintain the inside temperature.
Details of the balloon flight
Balloon launched on: 9/2/1965 at 2:28 utc
Launch site: Fleming Field Airport, South St.Paul, Minnesota, US
Balloon launched by: Winzen Research Inc.
Balloon manufacturer/size/composition: Zero Pressure Balloon Winzen - 325.000 cuft (1.5 mil Stratofilm)
Flight identification number: NYU 112
Balloon flight duration (F: time at float only, otherwise total flight time in d:days / h:hours or m:minutes - ): F 18 h 30 m
Campaign: Skyhook 65
Payload weight: 845 pds
- Atmospheric neutrons NASA Contractor Report 3126, May 1979
- Flight Record Scientific Ballooning Nº 21, December 1965
If you consider that this website is interesting or useful, you can help to keep it running with just the equivalent of the price of a cup of coffee. Click on the button on the right for more information.