| Every year since 1984, a student helicopter design competition has been co-sponsored by the American Helicopter Society, International, and the rotorcraft industry. Students from the University of Maryland first took part in 1988, placing third, but then remained absent from the competition for 10 years, until 1998, when Andy Bernhard and a group of other graduate students of the Alfred Gessow Rotorcraft Center revived interest in it. Since then, Maryland teams have participated every year, winning first place eight times in a row, over universities such as the Georgia Institute of Technology, the U.S. Naval Postgraduate School, and the U.S Air Force Institute of Technology. The students develop the design during the course of a one-semester class in Helicopter Design (ENAE 634) offered by the Department of Aerospace Engineering in the Spring of each year. The class is co-taught by Professor Inderjit Chopra, Senior Research Scientist Vengalattore Nagaraj, and Visiting Professor Marat Tishchenko [PDF link]. |
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| Year | Placed | The Design | Team Members | Summary | RFP | Report (pdf) | |
| 1988 | 3rd | N/A | N/A | N/A | Heavy-lift helicopter | N/A | N/A |
| 1998 | 1st | Chesapeake | ![]() |
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To develop a modern 12-seat civil VTOL transport rotorcraft with the capability to grow to 19 seats with minimum changes. | N/A |
(25 MB) (ps, 7 MB) |
| 1999 | 1st | CalVert | ![]() |
|
To develop a high-speed (180-kt cruise), VTOL, 4-6 place, personal transport aircraft, minimizing the the number of man hours required to fabricate the components. | (pdf, 1.9 MB) | (3 MB) |
| 2000 | 1st | MARV | ![]() |
|
To develop an autonomous rotorcraft for exploration of Mars. The mission was to be a proof-of-concept demonstration for rotary wing flight in the Martian atmosphere. |
(html) (doc, 32 KB) (pdf, 110 KB) |
(8 MB) |
| 2001 | 1st | Raven | ![]() |
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To develop a VTOL platform with an innovative method of controlling the cyclic pitch of the rotor blades. Methods that do not depend upon the use of traditional swashplate mechanisms were sought. |
(html) (doc, 82 KB) (pdf, 172 KB) |
(7 MB) |
| 2002 | 1st | TerpRanger | ![]() |
|
To upgrade and remanufacture a 4-6 place turbine helicopter for commercial applications, that can operate at 140 Kt cruise speed and have a range of 400nm. |
(html) (doc, 128 KB) (pdf, 199 KB) |
(4 MB) |
| 2003 | 1st | Aeneas | ![]() |
|
To design a VTOL urban disaster response vehicle for high rise firefighter deployment, rooftop occupant extraction, disaster command and control and other emergency response missions. |
(html) (doc, 693 KB) (pdf, 280 KB) |
(13 MB) |
| 2004 | 1st | Condor | ![]() |
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To develop a helicopter specifically designed for high altitude rescue operations. The aircraft had to be certified for single pilot, day/night operations with cruise speeds of at least 145 knots. | (pdf, 127 KB) |
(3.5 MB) (With bookmarks, 21 MB) |
| 2005 | 1st | Atlas | ![]() |
|
To design a military Heavy Lift VTOL aircraft that can operate from existing naval ships and transport a 20-ton FCS combat-ready vehicle. | (pdf, 493 KB) |
(6.5 MB) (Exec. summary, ppt, 7 MB) |
| 2006 | 2nd | Penguin / Pyros |
|
|
To design a two-seat, single-engine turbine training helicopter with operating characteristics representative of the [world's] turbine [helicopter] fleet, while being cost-competitive with current [piston-engined] training helicopters, along with the conceptual design of a low-cost turbine engine. | (pdf, 141 KB) |
(12 MB) (Exec. summary, ppt, 13.5 MB) |
| 2007 | 2nd | Triton | ![]() |
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To design an advanced manned VTOL Approach and Recovery Vehicle (ARV) that is capable of operating from a submersible vehicle in support of Special Operations Forces, and an advanced Unmanned Escort Vehicle (UEV) that is capable of supporting the operations of the ARV. | (pdf, 216 KB) |
(18 MB) (Exec. summary, ppt, 13 MB) |
| 2008 | -- | -- | -- | -- | To design an advanced, short-range, medium-speed, transport VTOL concept, capable of operating from an uprepared area, and which minimizes energy consumption and the complete pollution chain throughout the entire life cycle of the aircraft (manufacturing, operation, maintenance and end-of-life recycling), with initial operational capability (IOC) in 2020. | (pdf, 97 KB) | -- |
| * Team Leader |
| Last updated March 5, 2008 |
Questions / Comments:
Contact Jason Pereira (jpereira AT umd DOT edu) |