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'''Project SPACE (Space Payload) or SPCE''' is the Balloons team project to create a modular payload for high altitude balloon launches. The goal is to create a payload with interchangeable panels and floors so that groups that want to put experiments at near space on one of the balloons can easily modify individual small parts and be ready to launch very quickly.
'''Project SPACE (Systematic Platform for Advanced Customization and Effiency)''' is the Balloons team project to create a modular payload for high altitude balloon launches. The goal is to create a payload with interchangeable panels and floors so that groups that want to put experiments at near space on one of the balloons can easily modify individual small parts and be ready to launch very quickly.
The current team leads are Brandon Vabre and Yuji Sugimoto.
The current team leads are Brandon Vabre and Yuji Sugimoto.
== Origins ==
== Origins ==
Kirill Safin had the initial idea to create a modular payload for balloons launches.
Kirill Safin had the initial idea to create a modular payload for balloons launches with the intent of being able to swap out components as needed on a by-mission basis. Having to re-make a new styrofoam container for each launch seemed unnecessary, as only minor changes were made between payloads.
The initial goals for the payload were simply two pronged: to be able to modularly adapt to payload requirements, and to be thermally insulative. Finding a material that would be insulative and easy to work with was non-trivial; in the end, it was decided to pursue the route of High Density Polyurethane Foam (HDPU). This foam was known to have a thermal conductivity rating just below styrofoam, and was fully machineable to boot.
The principal design featured four main components - a ''chamber'', ''portals'', ''blocks'', and ''retainer plates''. The chamber was the skeleton of the payload, essentially a rectangular box out of HDPU foam panels epoxied together. The most notable aspect was the rounded square holes on each wall of the payload -- these were called ''portals''. A chamber had six portal of a pre-determined shape and size. The modular hot-swap ''blocks'' had the corresponding HDPU rounded-square panel. This HDPU block may or may not have been further machined depending on its purpose -- for example, a block meant to house a GoPro in one wall of the payload would also have a machined GoPro cavity and through-hole for the lens. However, other blocks, like the SSI logo block or note block did not require this kind of HDPU machining. The HDPU block was then epoxied to a wooden outer retention plate (initially bass wood). This outer retention plate had four 1/4" holes. When slotted into the appropriate chamber portal, the block was clamped to the payload using an internal retention plate and nylon bolts. All HDPU was also painted black for heat absorption.
SPACE Mk 1 flew on the first launch of 2015, housing SSI Gen 1 Avionics. It proved to be extremely thermally insulative (more than a styrofoam container) despite not being super air-tight, and allowed the modular swap of raspberry pi cameras, GoPros, logos, note blocks, and blank blocks. It's most profound drawback was its weight -- the total payload weighed in at around 2.5 kilograms.
A renewed emphasis on weight reduction led to the creation of SPACE Mk 2 - ''SPACE Micro''. This version of SPACE was dramatically smaller and less than half the weight. It utilized balsa wood instead of bass wood for weight reduction in paneling, and dramatically less HDPU. SPACE Micro was flown on seven SSI balloons, receiving tremendous usage by the team. It was ultimately abandoned for the lack of modularity needs at the given time. The creation of ValBal required a very specific thermal enclosure, with no modularity needs.