NASA Centurion

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Centurion
Centurion takes off from Dryden in December, 1998
Role Remote controlled UAV
Manufacturer AeroVironment
First flight November 10, 1998
Primary user NASA ERAST Program
Number built 1
Developed from NASA Pathfinder
Developed into
NASA Helios

The NASA Centurion was the third aircraft developed as part of an evolutionary series of

NASA Helios
.

Centurion

Quarter scale model of Centurion

Centurion, originally built for the 100,000 feet (30,000 m) altitude on solar power milestone specified by the ERAST project, was the third generation aircraft in the NASA Pathfinder series of electrical-powered flying wing unmanned aircraft. The ERAST program managers had determined that an aircraft based on the Pathfinder/Pathfinder Plus concept would be the lowest risk approach of achieving the altitude goal.[2]

Initially, a quarter-scale model of the Centurion was test flown at

Helios Prototype, with work starting in January, 1999.[1][2]

Aircraft description

The design of Centurion resulted in an aircraft that looked very much like the Pathfinder, but with a much longer wingspan of 206 feet (63 m). Although the Centurion shape resembled the Pathfinder, the structure was designed to be stronger and capable of carrying numerous payloads (up to 600 pounds (272.2 kg)) more efficiently. Its wing incorporated a redesigned high-altitude airfoil and the span was increased to 206 feet (63 m). The number of motors was increased to 14 and the number of underwing pods to carry batteries, flight control system components, ballast, and landing gear rose to four.[2]

Specifications

Solar Aircraft Evolution through the ERAST Program
Specifications[1][3][4][5]
  Pathfinder Pathfinder-Plus Centurion Helios HP01 Helios HP03
Length ft(m) 12 (3.6) 12 (3.6) 12 (3.6) 12 (3.6) 16.5 (5.0)
Chord ft(m) 8 (2.4)
Wingspan ft(m) 98.4 (29.5) 121 (36.3) 206 (61.8) 247 (75.3)
Aspect ratio 12 to 1 15 to 1 26 to 1 30.9 to 1
Glide ratio 18 to 1 21 to 1 ? ? ?
Airspeed kts(km/h) 15–18 (27–33) 16.5–23.5 (30.6–43.5) ?
Max altitude ft(m) 71,530 (21,802) 80,201 (24,445) n/a 96,863 (29,523) 65,000 (19,812)
Empty Wt lb(kg) ? ? ? 1,322 (600) ?
Max. weight lb(kg) 560 (252) 700 (315) ±1,900 (±862) 2,048 (929) 2,320 (1,052)
Payload lb(kg) 100 (45) 150 (67,5) 100–600 (45–270) 726 (329) ?
Engines electric, 2 hp (1.5 kW) each
No. of engines 6 8 14 14 10
Solar pwr output (kW) 7.5 12.5 31 ? 18.5
Supplemental power batteries batteries batteries Li batteries Li batteries, fuel cell

See also

References

This article contains material that originally came from the web article "Unmanned Aerial Vehicles" by Greg Goebel, which exists in the Public Domain. Public Domain This article incorporates public domain material from websites or documents of the

National Aeronautics and Space Administration
.

  1. ^ a b c "NASA Armstrong Fact Sheet: Helios Prototype". NASA. 13 August 2015. Archived from the original on 2023-04-19.
  2. ^ a b c NASA Centurion fact sheet, archived at archive.org, accessed September 8, 2008
  3. ^ NASA Pathfinder fact sheet, archived at archive.org
  4. ^ Investigation of the Helios Prototype Aircraft Mishap – Volume 1, T.E. Noll et al., January 2004
  5. ^ NASA Centurion Fact Sheet archived at archive.org

External links