"Pseudo-satellite" redirects here; not to be confused withPseudolite.
"Atmospheric satellite" redirects here; not to be confused withWeather satellite.
A high altitude platform can provide observation or communication services.
Ahigh-altitude platform station (HAPS, which can also meanhigh-altitude pseudo-satellite orhigh-altitude platform systems), also known asatmospheric satellite, is a longendurance, high altitudeaircraft able to offer observation or communication services similarly toartificial satellites. Mostlyunmanned aerial vehicles (UAVs), they remain aloft through atmospheric lift, eitheraerodynamic likeairplanes, oraerostatic likeairships orballoons.High-altitude long endurance (HALE)military drones can fly above 60,000 ft (18,000 m) over 32 hours, while civil HAPS areradio stations at an altitude of 20 to 50 km above waypoints, for weeks.
Stratospheric airships are often presented as a competing technology. However few prototypes have been built and none are operational.Among balloons specifically, the most well known high-endurance project wasGoogle Loon, using helium-filled high-altitude balloons to reach the stratosphere. Loon was ended in 2021.
High-altitude, long-endurance (HALE) aircraft are non-weaponizedmilitary drones capable of flying at 60,000 ft (18,000 m) over 32 hours, like the USAFRQ-4 Global Hawk or its variants used forISR.[1] This is above and longer thanMedium-Altitude, Long-Endurance (MALE) aircraft flying between 25,000 and 50,000 ft (7,600 and 15,200 m) during 24 hours, more vulnerable toanti-aircraft defense, like theUSAF ISR/strikeMQ-9 Reaper or its variants.[1]
High-altitude platform station (HAPS)
defined by theInternational Telecommunication Union (ITU) as "astation on an object at an altitude of 20 to 50 km and at a specified, nominal, fixed point relative to the Earth" in itsITU Radio Regulations (RR).[2] HAPS can also be the abbreviation forhigh-altitude pseudo-satellite.
In 1983,Lockheed producedA Preliminary Study ofsolar powered aircraft and Associated Power Trains for theNASA, as long endurance flight could be compared tosuborbital spacecraft.[3] In 1984 was published theDesign of Long Endurance Unmanned Airplanes Incorporating Solar andfuel cell propulsion report.[4] In 1989, theDesign and experimental results for a high-altitude, long-endurance airfoil report proposed applications as aradio relay, forweather monitoring or cruisemissile targeting.[5]
TheNASA ERAST Program (Environmental Research Aircraft and Sensor Technology) was started in September 1994 to study high-altitude UAVs, and was terminated in 2003.[6]In July 1996, the USAFStrikestar 2025 report forecast HALE UAVs maintaining air occupation with 24 hours flights.[7]TheDefense Airborne Reconnaissance Office made demonstrations of long-endurance UAV craft.[7]In September 1996,Israel Aircraft Industries detailed the design of a HALE UAV.[8]
In 2002,Preliminary reliability design of a solar-powered high-altitude very long endurance unmanned air vehicle was published.The European UnionCAPECON project aimed to develop HALE vehicles, while thePolish Academy of Sciences proposed its PW-114 concept that would fly at 20 km (66,000 ft) for 40 hours.[9]Luminati Aerospace proposed its Substrata solar-powered aircraft that wouldfly in formation like migratorygeese to reduce the power required for the trailing aircraft by 79%, allowing smallerairframes to remain aloft indefinitely up to a latitude of 50°.[10]
Wind profile variation with altitude from NASA, showing minimum wind speeds between 17 and 22 km (56,000 and 72,000 ft). Although absolute values will vary, the trends shown are similar for most locations.
Drag is reduced in thetropopause thin air, well above the 40–160 kn (74–296 km/h) high winds andair traffic of the hightroposphere between 20,000 to 35,000 ft (6,100 to 10,700 m).[13] Maintaining a position facing variable winds is a challenge.[14] Relatively mild wind andturbulence above thejet stream is found in most locations in thestratosphere between 17 and 22 km (56,000 and 72,000 ft), although this is variable with the latitude and season.[14] Altitudes above 55,000 ft (17,000 m) are also abovecommercial air transport.[14] Flying in thetropopause at 65,000 ft (20,000 m) is above clouds and turbulence with winds below 5 kn (9 km/h), and above FAA-regulatedClass A airspace ending at 60,000 ft (18,000 m).[11]
Comparison to satellites
A lower altitude covers more effectively a small region, implies a lower telecommunicationslink budget (a 34 dB advantage over aLEO, 66 dB overGEO), a lower power consumption, and a smallerround-trip delay.[15] Satellites are more expensive, take longer to deploy, and cannot be reasonably accessed for maintenance.[15] Asatellite in the vacuum of spaceorbits due to its high speed generating a centrifugal force matching the gravity. Changing a satellite orbit requires expending its extremely limited fuel supply.
HAPS can deliverradio connectivity to users, as an altitude above 12,500 m (41,000 ft) enableline-of-sight propagation of at least 400 km (220 nmi). HAPS could deliver bandwidth and capacity similar to abroadband wireless access network, likeWiMAX, over a coverage area similar to that of a satellite. Military communications can be improved in remote areas like in Afghanistan, where mountainous terrain interferes with communications signals.[17]
More than 90% of atmospheric matter is below the high-altitude platform, reducingatmospheric drag for starting rockets: "As a rough estimate, a rocket that reaches an altitude of 20 km (66,000 ft) when launched from the ground will reach 100 km (54 nmi) if launched at an altitude of 20 km (66,000 ft) from a balloon."[21]Mass drivers have been proposed for launching to orbit.[22][page needed]
Reconnaissance aircraft like the late 1950sLockheed U-2 could fly above 70,000 ft (21,000 m) and the 1964SR-71 above 80,000 ft (24,000 m).[13]The twin-turbofan poweredMyasishchev M-55 reached an altitude of 21,360 m (70,080 ft) in 1993, a variant of the M-17 first flown in 1982, which reached 21,830 m (71,620 ft) in 1990.
The mannedGrob G 520 first flew on 24 June 1987 and was certified in 1991. Powered by aHoneywell TPE331 turboprop, it is 33 m (108 ft) wide, reached 16,329 m (53,574 ft), and can stay airborne for 13 hours.
Capable of flying up to 60,000 ft (18,300 m) more than 34 hours, theRQ-4 Global Hawk was put intoUSAF service in 2001.
TheHALSOL prototype, a 185 kg (410 lb), 30 m (98.4 ft) wideflying wing propelled by eight electric motors, first flew in June 1983.[26] It joined theNASA ERAST Program in late 1993 as the Pathfinder, and with solar cells covering the entire wing added later, it reached 50,500 ft (15,400 m) on September 11, 1995 and then 71,530 ft (21,800 m) in 1997.[12] ThePathfinder Plus had four sections of the Pathfinder wing out of five attached to a longer center section, increasing span to 121 ft (37 m), it flew in 1998 and reached 80,201 ft (24,445 m) on August 6 of that year.[12]
Flying in late 1998, the Centurion had a redesigned high-altitude airfoil and span increased to 206 ft (63 m), 14 motors, four underwing pods to carry batteries, systems and landing gear.[12] It was modified into theHelios Prototype, with a sixth 41 ft (12 m) wing section for a 247 ft (75 m) span, and a fifth landing gear and systems pod. It first flew in late 1999, solar panels were added in 2000 and it reached 96,863 ft (29,524 m) on August 13, 2001.[12] A production aircraft would fly for up to six months.[12] It broke up in flight in 2003.[27]
Airbus Zephyr
TheZephyr were originally designed byQinetiQ, a commercial offshoot of theUK Ministry of Defence.[28] The UAVs are powered bysolar cells, rechargingbatteries in daylight to stay aloft at night. The earliest model flew in December 2005.[29] In March 2013, the project was sold toAirbus Defence and Space.[30] The latest Zephyr 8/S model weighs 75 kg (165 lb), has a wingspan of 25 m (82 ft), and reached 23,200 m (76,100 ft).[31]
Solar Impulse
The firstSolar Impulse manned demonstrator made its first flight on 3 December 2009, and flew an entire diurnal solar cycle in a July 2010 26-hour flight. The 71.9 m (236 ft) wide, 2.3 tonnes (5,100 lb) Solar Impulse 2 first flew on 2 June 2014, it could reach 12,000 m (39,000 ft) and its longest flight was fromNagoya, Japan toKalaeloa, Hawaii over 117 h 52 min on 28 June 2015.
Titan Aerospace Solara
Founded in 2012 inNew Mexico,Titan Aerospace was developing largesolar-powered, high-altitude atmospheric satellites similar to theAeroVironment Global Observer orQinetiQ Zephyr.[11] Their wing, over 160 ft (50 m) wide, would be covered withsolar cells to provide energy for day flight, stored inelectric batteries for use at night.[11] Costing less than $2 million, they could carry a 70 lb (30 kg) payload for up to five years, limited by battery deterioration.[11] In 2013, Titan was flying two fifth-scale test models and aimed to flight test a full-sized prototype by 2014.[11] In March 2014,Facebook was interested in the company, led at the time byEclipse Aviation founder Vern Raburn, for $60 million.[16]Google bought Titan Aerospace in April 2014,[32] managed to fly a prototype in May 2015 but it crashed within minutes and Titan Aerospace was shut down by early 2017.[33]
TheKARI EAV-3 flew during 53 hours and up to 22 km (72,000 ft).
KARI EAV
TheKorea Aerospace Research Institute (KARI) began developing its Electrical Aerial Vehicle (EAV) in 2010, after subscale demonstrators, its latest 20 m (66 ft) wide EAV-3 weighs 66 kg (146 lb) and is designed to fly for months; it flew up to 14.2 km (47,000 ft) in August 2015, during 53 hours and up to 22 km (72,000 ft) in August 2020.[34]
Astigan A3
UK mapping agencyOrdnance Survey (OS), a subsidiary of theDepartment for Business, Energy & Industrial Strategy, is developing the A3, a 38 m (125 ft) wingspan, 149 kg (330 lb) twin-boom solar-powered HAPS designed to stay aloft at 67,000 ft (20,000 m) for 90 days carrying a 25 kg (55 lb) payload.[35] OS owns 51% of UK companyAstigan, led byBrian Jones, developing the A3 since 2014 with scale model test flights in 2015 and full-scale low-altitude flights in 2016.[35] High-altitude flights should begin in 2019, to complete tests in 2020 with a commercial introduction as forenvironmental monitoring,mapping, communications and security.[35] In March 2021, the project was ended as no strategic partner was found.[36]
Facebook Aquila
TheFacebook Aquila UAV was a carbon fiber, solar-poweredflying wing UAV spanning 132 ft (40 m) and weighing 935 lb (424 kg), designed to stay aloft at FL650 for 90 days.[27] It was designed and manufactured by UK company Ascenta forFacebook, to provide internet connectivity.[37] UAVs would useLaser communication between them and to ground stations.[38] On June 28, 2016, it took its first flight, during ninety minutes and reaching 2,150 ft (660 m), but a twenty-foot section of the righthand wing broke off during final approach.[39][40] It made another low-altitude test flights in 2017.[27] On June 27, 2018, Facebook announced it will halt the project and plan to have other companies build the drones.[41]
China Aerospace Science and Technology Corporation
CASTC flew a 147 ft (45 m)-span solar-powered UAV to FL650 in a 15 hours test flight in July 2017.[27]
Lavochkin LA-252
Russia'sLavochkin design bureau is flight-testing the LA-252, an 82 ft (25 m)-span, 255 lb (116 kg) solar-powered UAV designed to stay aloft 100 days in the stratosphere.[27]
Mira Aerospace ApusDuo
A joint venture between Abu Dhabi-basedBayanat AI and American UAV manufacturerUAVOS,Mira Aerospace'sApusDuo HAPS has completed over 100 test flights across 3 continents, building off technologies first developed in 2014.[42][not specific enough to verify] With a wingspan of 14 m (46 ft), the unmanned ApusDuo 14 aircraft utilizes a flexibletandem wing design with high-efficiency solar cells to fly continuously for months at altitudes up to 19,000 m (62,000 ft), carrying payloads up to 6 kg (13 lb). During a test flight in Rwanda in October 2023, Mira Aerospace became the first company to successfully deliver5G connectivity from a fixed-wing HAPS autonomous aircraft in the stratosphere.[43]
Aurora Odysseus
Aurora Flight Sciences announced itsOdysseus in November 2018.[44] The 74.1m (243ft) widecarbon fibre aircraft weigh less than 880 kg (1,940 lb) and can carry a 25kg (55lb) payload.[45] It was designed to stay above 65,000 ft (20,000 m) up to three months at latitudes up to 20°.[46] Its first flight was indefinitely delayed by July 2019.[44]
AeroVironment HAPSMobile
AeroVironment will design and development solar-powered UAV prototypes for $65 million forHAPSMobile, a joint venture 95% funded and owned by Japanese telcoSoftBank.[27] Resembling the 1999Helios, the 256 ft (78 m) spanflying wing with 10 electric-driven propellers would provide4G LTE and5G direct to devices over a 200 km (125 mi) diameter area[47] On 21–22 September 2020, the HAPSMobile Hawk30 (rebranded asSunglider) flew 20 hours and reached an altitude of 62,500 ft (19,000 m), testing the long-distanceLTE communications developed with Loon for standard LTEsmartphones andwireless broadband communications.[48]
BAE Systems PHASA-35
Designed by Prismatic Ltd., nowBAE Systems, the 35 m (115 ft)-wingspanBAE Systems PHASA-35 made itsmaiden flight in February 2020 from theWoomera Test Range in South Australia; it should fly its 15 kg (33 lb) payload at around 70,000 ft for days or weeks.[49] By December 2024, it had flown for 24h and reached more than 66,000 ft (20,000 m) fromSpaceport America in New Mexico, targeting operational activity by 2026.[50]
Swift Engineering SULE
TheSwift Engineering's Swift Ultra Long EnduranceSULE completed its maiden flight partnership withNASA's Ames Research Center in July 2020.[51] Designed to operate at 70,000 ft (21,000 m), the persistent 72 ft (22 m) UAV weighs less than 180 lb (82 kg) and can carry up to 15 lb (6.8 kg) payloads.[51] On Sep. 29-30, 2024, it reached 55,904 ft (17,040 m) in a 24-hour flight.[52] It took off from and landed atSpaceport America in New Mexico.[53]
HAL CATS Infinity
CATS Infinity is being developed byHAL,NAL and NewSpace Research. Its scaled down model first flew in 2022. In February 2024, the 23 kg (51 lb) scaled down prototype with a 12 m (39 ft) wingspan reached 3,000 m (9,800 ft) fromChitradurga Aeronautical Test Range during eight and a half hours, development completion was then expected for 2027.[54][better source needed] In May 2024, the scaled down prototype flight tests reached 26,000 ft (7,900 m) during 27 hours from Chitradurga.[55] The subscale prototype has a goal of a 7-day flight at an altitude of 20 km (66,000 ft) cruising at 100 km/h (54 kn).[citation needed] The full-scale, 450 kg (990 lb) CATS Infinity target is a ninety-day endurance at high altitudes, with a 35 kg (77 lb) payload.[citation needed] The Indian Navy is also interested in this project.[56]
Kea Atmos Mk1
The Kea Atmos Mk1 solar-powered stratospheric HAPS was designed and manufactured byKea Aerospace in New Zealand. The maiden test flight was in February 2023 and the first stratospheric flight was on February 8, 2025. It has a wingspan of 12.5 meters and weighs less than 40 kg. The Kea Atmos Mk1 is designed to take 2 kg payloads to the stratosphere on dawn to dusk single day missions and is working with a range of international payload customers. Kea Aerospace is currently designing the Kea Atmos Mk2 to take 6 kg of payload to the stratosphere on multi-month length missions.[citation needed]
TheRyan YQM-98 R-Tern of the Compass Cope program first flew on 17 August 1974 and was designed to fly up to 70,000 ft (21,340 m) and during 30 hours
USAF Compass Dwell and Compass Cope
The USAF Compass Dwell UAV program saw the flight of theLTV XQM-93 in February 1970, based on a turboprop-poweredSchweizer SGS 2-32 sailplane and designed to fly 24 hours and to reach 50,000 ft (15,240 m); and theMartin Marietta Model 845 in April 1972, based on a piston engine-poweredSchweizer SGS 1-34 sailplane, designed to reach 40,000 feet (12,000 m) and capable to fly 28 hours. The following Compass Cope program saw theBoeing YQM-94 B-Gull first flight on 28 July 1973: powered by aGeneral Electric J97 turbojet, it was designed to fly 30 hours up to 70,000 ft (21,340 m), and managed to fly during 17.4 hours and up to 55,000 feet (16,800 m); the competingRyan YQM-98 R-Tern was powered by aGarrett ATF3 turbofan, first flew on 17 August 1974 and was designed to fly during 30 hours.
Boeing Condor
TheBoeing Condor first flew on October 9, 1988, it reached 67,028 ft (20,430 m) and stayed aloft for nearly 60 hours; powered by two 175 hp (130 kW) piston engines, the 200 ft (61 m) wide UAV had a 20,300 lb (9,200 kg) gross weight and was designed to reach 73,000 ft (22,250 m) and to fly for more than a week.[57]
Aurora Perseus and Theseus
Built byAurora Flight Sciences for what would become theNASA ERAST Program, the Perseus Proof-Of-Concept UAV first flew in November 1991 followed by Perseus A on 21 December 1993, which reached over 50,000 ft (15,000 m). Designed to fly at 62,000 ft (18.9 km) and up to 24 hours, Perseus B first flew on 7 October 1994 and reached 60,280 ft (18,370 m) on June 27, 1998. Itspusher propeller is powered by aRotax 914 piston engine boosted by a three-stage turbocharger flat-rated to 105 hp (78 kW) to 60,000 ft (18,000 m). It has a 2,500 lb (1,100 kg) maximum weight, is able to carry a 260 lb (120 kg) payload and its 71.5 ft (21.8 m) wing has a high 26:1aspect ratio.[58] A larger follow-on powered by twoRotax 912 piston engines, the Theseus first flew on May 24, 1996. Designed to fly during 50 hours up to 65,000 ft (20,000 m), the 5,500 (2.5 t) maximum weight UAV was 140 ft (42.7 m) wide and could carry a 340 kg (750 lb) payload.[6]
Grob Strato 2C
Designed to fly at 24,000 m (78,700 ft) and for up to 48 hours, the mannedGrob Strato 2C first flew on 31 March 1995 and reached 18,552 m (60,897 ft). The 56.5 m (185 ft) wide aircraft was powered by two 300 kW (400 hp) piston engines turbocharged by aPW127 turboprop as the gas generator.
The piston-poweredGeneral Atomics Altus II first flew on May 1, 1996, and reached 57,300 ft (17,500 m)
General Atomics ALTUS
Part of theNASA ERAST Program, the high-altitude UAVGeneral Atomics ALTUS I & II were civil variants of theGnat 750 (which also spawned the USAFPredator A) which had a 48 hours endurance, with a longer wingspan at 55.3 ft (16.9 m). Powered by a 100 hp (75 kW) turbochargedRotax 912 piston engine, The 2,130 lb (970 kg) MTOW testbed could carry up to 330 lb (150 kg) of scientific instruments. The Altus II first flew on May 1, 1996, had an endurance over 26 hours, and reached a maximumdensity altitude of 57,300 ft (17,500 m) on March 5, 1999. They led to the larger, turboprop-poweredGeneral Atomics Altair.[59]
Scaled Composites Proteus
The mannedScaled Composites Proteus operates at altitudes of 19.8 km (65,000 ft), while carrying a 1,100 kg (2,400 lb) payload.[60] Powered by twoWilliams FJ44 turbofans, it hadtandem wings with a 17 m (55 ft) front wing and a wider 24 m (78 ft) wide back wing for a maximum takeoff weight of 6.6 t (14,500 lb), could cruise at 450 km/h (240 kn) and stay 22 hours at 925 km (500 nmi) of its base.[6]
Virgin Atlantic GlobalFlyer
The mannedGlobalFlyer, built byScaled Composites, was designed to fly around the world. Powered by a singleWilliams FJ44, the 114 ft (35 m) wide aircraft can weigh up to 22,100 lb (10 t). Having a 50,700 ft (15,450 m) ceiling, it flew for 76 hours and 45 minutes in February 2006.
Aurora Flight Sciences Orion
The initial Boeing/Aurora Flight Sciences Orion platform would cruise at 65,000 ft (20,000 m) for 100 hours, powered byliquid hydrogen feedingpiston engines; its takeoff weight of 7,000 lbs (3.2 tons) allowing 400 lbs (180 kg) payloads.[13] It evolved into a twin turbo-diesel-poweredMALE UAV burning jet fuel with an increased gross weight to 11,000 lb (5,000 kg), designed to fly at 20,000 ft (6,100 m) during 120 hours (five days) with a 1,000lb payload, or a week with a smaller one; it made its first flight in August 2013 and flew during 80 hours in December 2015, landing with enough fuel for 37 hours more.[61]
Fueled byliquid hydrogen and designed to fly at up to 65,000 ft (20,000 m) for up to 7 days, theAeroVironment Global Observer first flew on 5 August 2010.[64] After a crash in April 2011, the Pentagon shelved the project.[65]
Boeing Phantom Eye
An evolution of theBoeing Condor developed byBoeing Phantom Works, theBoeing Phantom Eye first flew in June 2012.[66] Powered by two 150 hp (110 kW) turbocharged Ford 2.3 literpiston engines running on liquidhydrogen, the 150 ft (46 m) wide UAV has a gross takeoff weight of 9,800 lbs (4.4 t) and can carry a 450 lb (200 kg) payload.[66] It cruises at 150 kn (280 km/h), can reach 65,000 ft (19,800 m) and have a four days endurance.[66] A full size variant is designed to carry a 2,000 lb (910 kg) payload during ten days.[66] In August 2016, the Phantom Eye demonstrator was transferred to theAir Force Flight Test Museum.[67]
Stratospheric Platforms
UKStratospheric Platforms, created in 2014, went public on 19 October 2020; after flight trials of a 4G/5G relay on aGrob G 520 at 45,000 ft (14,000 m), the start-up is developing a hydrogen-fuel cell-powered HAPS UAV built byScaled Composites, with a wingspan of 60 m (200 ft), that would fly at 60,000 ft (18,000 m) for nine-days with a payload of 140 kg (310 lb).[68]
Unmannedstratospheric airships are designed to operate at very high 60,000 to 75,000 feet (18.3 to 22.9 km) altitudes during weeks, months or years.[69]Subjected toultraviolet damage,ozone corrosion and challenging station keeping, they can be solar-powered withenergy storage for the night.[69]
The first stratospheric powered airship flight took place in 1969, reaching 70,000 feet (21 km) for 2 hours with a 5 pounds (2.3 kilograms) payload.[70]By August 2002, US companyWorldwide Aeros was building a stratospheric demonstrator for theKorea Aerospace Research Institute, as a part the South Korean HAA development program.[71]By April 2004, stratospheric airships were being developed in USA, UK, Canada, Korea and Japan.[72]In May 2004, theJapan Aerospace Exploration Agency shown its test airship inTaiki, Hokkaido, a part of its Stratosphere Platform Project.[73]
SwRI HiSentinel
On December 4, 2005, a team led bySouthwest Research Institute (SwRI), sponsored by the Army Space and Missile Defense Command (ASMDC), successfully demonstrated powered flight of theHiSentinel stratospheric airship at an altitude of 74,000 feet (23 km).[74]
The United States Department of DefenseMissile Defense Agency contractedLockheed Martin to build an unmannedHigh-Altitude Airship (HAA) for itsBallistic Missile Defense System.[75] In January 2006, Lockheed won a $149M Contract to build it and demonstrate its technical feasibility and military utility.[76] It would operate above 60,000 ft (18,000 m) in a quasi-geostationary position to deliver persistentorbital station keeping as asurveillance aircraft platform, telecommunications relay, or a weather observer. Launch was originally proposed in 2008, the production aircraft would be 500 ft (150 m) long and 150 ft (46 m) in diameter. Powered by solar cells, it would stay in the air for up to one month and was intended to survey a 600 mi (970 km) diameter of land.
Lockheed-Martin HALE-D
On July 27, 2011, the "High Altitude Long Endurance-Demonstrator" (HALE-D) subscale demonstrator was launched on a test flight.[77] HALE-D had a 500,000 cu ft (14,000 m3) volume, was 240 ft (73 m) long and 70 ft (21 m) wide, had 15 kW (20 hp) solar cells charging 40 kWh Li-ion batteries and 2 kW (2.7 hp) electric motors to cruise at 20 kn (37 km/h)TAS at 60,000 ft (18,000 m) with a 50 lb (23 kg) payload during 15 days.[78] At 32,000 ft (9,800 m) a problem with the helium levels prevented it and the flight was terminated.[79] It descended and crashed in aPittsburgh area forest.[80] Two days after, it was destroyed by a fire before its recovery.[81]
Lindstrand HALE airship
Lindstrand Technologies designed aHelium-fillednon-rigid airship covered with solar cells. The 14 t (31,000 lb) aircraft could carry a 500 kg (1,100 lb) payload during 3 to 5 years as helium loss would be minimal at high altitudes. For energy storage, a 180kWelectrolyser would fill H2 and O2 tanks, to be converted back to water by a 150kWfuel cell. An 80 kW (110 hp) motor would allow a 24 m/s (47 kn) maximum speed.[82]
Stratobus airship
Thales Alenia Stratobus
Thales Alenia Space develops the Stratobus unmanned, solar-powered stratosphericairship, 377 ft (115 m) long and weighting 15,000 lb (6,800 kg) including a 550 lb (250 kg) payload, it is designed for a five-year mission with annual servicing and a prototype was planned for late 2020.[27]
H-Aero
H-Aero LTA-based launch systems for Mars exploration,[83] with development taking place via terrestrial high-altitude platforms. The first systems were tested by 2021.[84][better source needed]
Stratoship SZ-155
The SZ-155 was designed and manufactured by Stratoship in Australia. The SZ-155 flew two low altitude test flights in 2022 and 2024 before reaching the stratosphere on its first high altitude flight on May 5th, 2025. It flew for 11 hours and 12 minutes in total, and spent over 8 hours in the stratosphere. The SZ-155 is 25 meters long and was designed for flights of up to 7 days endurance. It can carry up to 10kg of payload to the stratosphere. Stratoship is currently designing a future model for multi-month flights.
Ageostationary balloon satellite (GBS) flies in thestratosphere (60,000 to 70,000 ft (18 to 21 km) above sea level) at a fixed point over the Earth's surface. At that altitude the air has 1/10 of itsdensity is atsea level.A GBS could be used to providebroadband Internet access over a large area.[85]One prior project was theGoogle'sProject Loon, which envisioned using helium-filledhigh-altitude balloons.
TheBoeing A160 Hummingbird is a rotorcraft produced by Boeing.[86] First flown in 2002, the program had goals of a 24-hour endurance, and 30,000 ft (9,100 m) altitude, but was abandoned in December 2012.
^Singer, Cs (June 2012). "Ultralight Solar Powered Hybrid Research Drone".Concepts and Approaches for Mars Exploration.1679: 4059.arXiv:1304.5098.Bibcode:2012LPICo1679.4059S.
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