The Japanese American Collaborative Emulsion Experiment (JACEE) was a scientific effort carried out to measure the composition and spectra of primary cosmic rays at the top of the atmosphere, using emulsion chambers transported by stratospheric balloons. JACEE's first flight was conducted in 1979, and flights continued through 1996, totaling 14 flights and 13 successful missions. The collaboration leveraged Japanese expertise in photographic materials and microscopy, American expertise in ballooning and data analysis, and Polish resources in scanning and measurement of emulsions.
Each payload could contain one, three, or four chambers, each chamber with an area about 2000 cm2, 12~25 cm thick, and weighing ~120 kg. Figure at left shows a schematic diagram of the vertical configuration of one chamber. It was comprised of four sections, identifiable according to their function in the experiment. These are, from the top, the charge detector, the target, the spacer, and the calorimeter. All sections were multilayered stacks of track-sensitive materials (emulsions, x-ray films, CR-39, Lexan) alternated with absorbers (acrylic, lead). There were approximately 300 layers of emulsion in the chamber. This configuration was more or less the same for all the flights. However, many flights not included the spacer section, and in some cases were added other elements like Cerenkov detectors or plastic scintillators.
The charge detector employed thick (200 - 400 micron) emulsions, which permited accurate determination of the charge of each primary particle via measurements of the grain density, gap distribution, and/or delta ray distribution. The target section was comprised basically of thin (50 ~ 75 micron) emulsion plates alternated with acrylic sheets. The substantial mass of low-Z material maximized the interaction probability, while the emulsion optimized the observation of charged tracks from an interaction vertex. In order to identify nuclear fragments, charge identification layers composed of thick emulsions and etchable plastics were inserted at regular intervals throughout the target.
The spacer section consisted of honeycomb paper with a few thin emulsions positioned at regular intervals that facilitated the tracing of tracks through it. Finally, the calorimeter was the energy measuring portion of the apparatus. It consisted of 1.0 and 2.5 mm thick lead sheets alternating with thin emulsion plates and x-ray films. Gamma rays emanating from a vertex in the target initiated electro-magnetic cascades in the calorimeter. The cascades produced dark spots in the x-ray films, the observation of which provided the trigger for an event. The events were traced back from the calorimeter, through the spacer, to the vertex in the target by observing associated tracks in the emulsions.
All flights made in Antarctica for JACEE after 1992 used the same gondola design: a simple, lightweight and very rugged framework that provided protection for the emulsion chamber modules in case of an awkward landing or parachute drag, wich also was easy to dissasemble on the landing spot or to be replaced in short notice at a low cost. The payload included an onboard data logging computer which was an adaptation of electronics originally designed for other project to record pressure altitude and module temperatures. The JACEE data logger was interfaced to the NSBF SIP (Support Instrument Package) allowing status monitoring and data downloading during flight.
Launch site: Williams Field, McMurdo Station, Antarctica
Balloon launched by: National Scientific Balloon Facility (NSBF)
Balloon manufacturer/size/composition: Zero Pressure Balloon SF3-424.37-080-NSCR-X-ST
Balloon serial number: W29.47-2X-04
Flight identification number: 374NT
Payload weight: 3007 lbs
Overall weight: 4236 lbs
The balloon was launched by dynamic method on December 14, 1993. After a nominal climb to float altitude it started a counter clock-wise path over Antarctica. The complete turn around the south pole was completed on December 23. At that moment was decided to terminate the flight once it passed McMurdo station.
The termination command was sent at 6:43 utc but it failed, so it was decided to bring it down valving the helium inside the envelope. By the moment that the balloon reached ground level it had drifted from the planned landing location and cleared the sea shore. The payload crashed through the ice and sunk only one quarter mile offshore of Ross Island. Intitially attempts to dredge for the gondola were made in the next days but did not succeed.
A year later, in Febraury 1995 another recovery operation was carried out using the PALMER icebreaker. Starting from the last known GPS position of the payload, the ship mapped the depth profile of the entire Wohlschlag Bay, to find best paths to use a towed high resolution sidescan sonar. Then when two or three possible candidates of JACEE-11's resting place were pinpointed, a line would be towed to hook up the package. However, bad weather and the presence of Icebergs in the zone forced to abort the recovery effort for the season. No recovery would be attempted in following campaigns so the payload was declared lost.
Post flight analysis traced the error to a mechanical failure in the termination mechanism which cuts the payload and its parachute from the balloon upon command from the ground station. A thorough investigation by NASA revealed that parts used in the mechanism had not been machined to design specifications.
It's worth to mention that the 1993/1994 NASA balloon launch season in Antarctica was the first time that two JACEE payloads where flown. Following the failure of this mission, the second launch of the campaign (JACEE-12) in January 1994 was a total success logging more than 210 hours of continued exposure of the emuslion chambers.