Purpose of the flight and payload description

The StratEx mission, officially known as the Stratospheric Exploration project, aimed to develop a system enabling an individual to ascend to, explore, and safely return from the stratosphere. This system was analogous to a SCUBA suit designed for underwater exploration, focusing on simplicity, safety, and lightweight design compared to traditional capsule-based systems. Conceptualized in December 2011 by Alan Eustace, Senior Vice President of Knowledge at Google Inc. pilot and an avid skydiver in collaboration with Paragon Space Development Corporation, the mission sought to address the feasibility of creating a self-contained system for human stratospheric exploration.

The StratEx mission employed an intricate array of hardware to ensure a successful and safe stratospheric flight and descent. In the image at left can be seen the suit in launch position (click for more details). Central to the system was the Pressure Suit Assembly (PSA), which encompassed a pressure suit, equipment module (EM), and the flight recovery system. The suit was designed to maintain a pressurized environment at 37.2 kPa, protect the pilot from extreme stratospheric conditions, and integrate with environmental control and life support systems (ECLSS). It featured a Dual Suit Controller (DSC) to manage internal pressure, a Demand Helmet Regulator (DHR) for oxygen delivery, and a liquid thermal garment (LTG) to regulate temperature. The helmet bubble included anti-glare features and ensured clear visibility. Mounted on the pilot's chest, the EM housed high-pressure oxygen tanks, batteries, and a heat exchanger system to manage temperatures, alongside avionics for navigation, telemetry, and communication.

The flight recovery system, critical for descent, included a drogue parachute for stabilization, a main parachute for controlled landing, and a backup parachute activated either manually or via an Automatic Activation Device (AAD) in emergencies. The innovative Stiff Anti-Entanglement Bridle Ejecting Rod (SAEBER) system prevented entanglement during drogue deployment. Ground support was facilitated by the Ground Cart (GC), which provided oxygen, cooling, and electrical power before liftoff, maintaining consumables and system functionality until launch.

The Flight Vehicle, a helium balloon, was engineered to lift the pilot to the stratosphere. Its envelope, constructed of specialized polyethylene, included a servomotor-controlled crown valve for helium venting and a reinforced base fitting for equipment attachment. The Balloon Equipment Module (BEM), suspended below, housed avionics, radar reflectors, and telemetry systems. It featured a destruct system for safe decommissioning post-mission, using a weighted tear mechanism or a fuse-activated release. The BEM also carried ballast to adjust ascent rates and housed video transmission systems to relay real-time visuals.

The Launch System involved extensive ground-based support infrastructure, including the balloon support equipment for safe handling and inflation, helium supply systems, and a ''Spork" vehicle to raise the balloon into position. A launch plate and sedan ensured the balloon and pilot were securely stationed during the launch process, with equipment enabling controlled lateral movement as the balloon ascended.

Mission Control integrated hardware and software for real-time monitoring and coordination, with personnel overseeing pilot health, ECLSS performance, and flight trajectory. Redundant communication systems ensured continuous connectivity. The Chase and Recovery system utilized helicopters, trucks, and fixed-wing aircraft, supported by GPS navigation, to track and recover the pilot and equipment efficiently. The medical team and technicians were equipped to handle contingencies, including pilot extraction and post-landing support.

The StratEx mission hardware demonstrated a sophisticated balance of innovation, redundancy, and operational precision, enabling groundbreaking exploration of the stratosphere.

Video footage from the third jump of StratEx mission

Details of the balloon flight

Balloon launched on: 10/24/2014 at 7:00 mdt
Launch site: Roswell Industrial Air Center, New Mexico, US  
Balloon launched by: PARAGON
Balloon manufacturer/size/composition: Zero Pressure Balloon 11.000.000 cuft
End of flight (L for landing time, W for last contact, otherwise termination time): 10/24/2014 at 9:24 mdt
Balloon flight duration (F: time at float only, otherwise total flight time in d:days / h:hours or m:minutes - ): 2 h 23 m
Landing site: 70 miles from Roswell, New Mexico, US

This was the third and final crewed flight of the program. The 328,000 m³ helium balloon was launched on October 24, 2014, from Roswell International Air Center in New Mexico, carrying pilot Alan Eustace, equipped with a custom space suit integrated with essential life-support systems. After ascending to a peak altitude of 41,578 meters (136,410 feet), Eustace detached from the balloon at 41,422 meters (135,899 feet). During his descent, stabilized by a small drogue parachute, he reached speeds of 1,320 km/h (Mach 1.22) in a freefall that lasted 4 minutes and 27 seconds, covering a vertical distance of 37,623 meters (123,435 feet) before deploying his main parachute. Eustace safely landed 125 kilometers east of the launch site.

StratEx set multiple world records, including the highest altitude for a manned balloon flight and the longest freefall distance with a drogue chute. It demonstrated a robust and reusable system for high-altitude exploration, receiving recognition such as the Smithsonian's inclusion of the StratEx system in its National Air and Space Museum collection and a nomination for the 2014 Collier Trophy. The mission's success also highlighted its potential applications in fields like commercial spaceflight and atmospheric research.

External references

Images of the mission

         

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