The Thunderhead Balloon System is a steerable multipurpose platform developed by Raven Aerostar for stratospheric missions of long duration, with navigational capabilities and the ability of performing persistent flight over areas of interest. The balloons can be flown individually or in constellations to support a wide range of requeriments including intelligence, surveillance, and reconnaissance; serve as an alternative to satellite communications or make surveys of ground, marine and environmental objectives.
The heart of the system is a superpressure balloon to which is attached a gondola containing the payload, flight systems and solar panels.
The balloon is a pumpkin-shaped superpressure model made of polyethylene in several sizes with a volume varying from 64.000 cubic feet to 400.000 cubic feet and altitudes of flight of between 50 and 65 kft for the smaller ones and between 75 and 92 kft for the bigger ones. This is well above commercial jetliners and weather phenomena. Both models can carry a payload of up to 125 pounds. To inflate the balloon is used helium and once it reach float altitude it expands and pressurises acquiring the final pumpkin shape. Inside the main balloon there is a smaller one called "balloonet" which serves as ballast and is the heart of the Thunderhead steering system: air is introduced into it using a special built pump permitting the balloon to modify its weight for ascent or descent. Although is not possible to directly control course or speed, these altitude changes allows the balloon to take advantage of different wind patterns at different altitudes for navigation. The balloon is also equipped with a valve at the top which is used to introduce helium during inflation and to vent helium during flight. The average flight duration can range from a few days to two months.
The instrumented gondola is attached directly below the balloon. Is composed of lightweight materials, may vary in size and can be rectangular shaped or truncated pyramid shaped. The upper part of the gondola houses in an insulated compartment the avionics and the elements that are part of the command and control system: ADS-B Out transponder for localization by nearby planes and Air Traffic controllers; RF-based systems for LOS (Line Of Sight) communications; Iridium-based system for BLOS (Beyond Line Of Sight) communications; GPS aided inertial navigation systems for real time positioning and Iridium backhaul as datalink for control and command of the payload. On the sides of this compartment are mounted the solar panels which varies in size according to power requeriments. They provide energy to the whole system during the day while charging onboard batteries for nighttime operations. Protruding ends of the booms on which are mounted the panels also serve to mount GPS and Iridium antennas. In some cases an additional payload compartment is located directly below the instrumented gondola with size and shape specially adapted for the mission requirements. If necessary, insulating panels can be added on the sides to protect onboard equipment and help to counteract the extremes temperatures of the stratosphere. A packed parachute is attached between the bottom of the balloon and the top of the gondola to allow a safe descent of the equipment at mission's end. In some cases, crush pads are fixed to the bottom of the gondola to absorb the shock of the landing.
Thunderhead systems are highly versatile with minimal space requirements for ground operation, so they can be launched by semi-manual means or using specially developed mobile platforms from almost anywhere, including small airfields, open terrain, or even from any vessel in open sea.
Balloon launched on: 11/8/2024 at 15:00 UTC
Launch site: Hurley, South Dakota, US
Balloon launched by: Aerostar
Balloon manufacturer/size/composition: Superpressure balloon with internal ballonet
Flight identification number: HBAL647
End of flight (L for landing time, W for last contact, otherwise termination time): 12/6/2024
Balloon flight duration (F: time at float only, otherwise total flight time in d:days / h:hours or m:minutes - ): 28 d
Landing site: Last known position was over the Guinea Gulf
OBJECTIVE OF THE FLIGHT
The balloon mission was undertaken by Airbus U.S. Space & Defense and Aerostar focused on testing satellite backhaul technologies for stratospheric intelligence, surveillance, and reconnaissance (ISR). It utilized Aerostar's stratospheric balloons equipped with cutting-edge technological systems to explore the potential of high-altitude platforms in ISR applications. The mission's goal was to evaluate the performance and reliability of satellite backhaul communication systems in the stratosphere, particularly for applications where persistent and secure data transmission is critical.
Aerostar's Thunderhead balloon served as platform to carry payloads into the stratosphere, operating at altitudes of approximately 65,000 feet. The payloads included advanced communication equipment designed to connect with satellites, ensuring the ability to transmit data securely and efficiently between the balloon and ground stations or other assets in a network.
One of the core technologies tested was the integration of stratospheric platforms with satellite communication systems. This required precise engineering to ensure compatibility and seamless operation in a challenging environment. The payloads needed to withstand extreme temperatures, low pressures, and high levels of solar radiation. Additionally, they were designed to minimize weight and power consumption while maximizing performance.
Another critical aspect was the data security protocols implemented for the satellite backhaul systems. The mission aimed to evaluate encryption methods and network resilience to cyber threats, given the sensitivity of ISR applications. The ability to transmit high-bandwidth data securely and with low latency was a primary focus.
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