Dynamically Scaled Modular Aircraft for Flight-Based Aviation Safety Research

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$699,962.00
Award Year:
2013
Program:
SBIR
Phase:
Phase II
Contract:
NNX13CL58C
Award Id:
n/a
Agency Tracking Number:
114637
Solicitation Year:
2011
Solicitation Topic Code:
A1.15
Solicitation Number:
n/a
Small Business Information
GA, Kennesaw, GA, 30144-3636
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
829299747
Principal Investigator:
Nicholas Alley
Principal Investigator
(678) 594-5227
nalley@areai.aero
Business Contact:
Nicholas Alley
Business Official
(678) 594-5227
nalley@areai.aero
Research Institute:
Stub




Abstract
Area-I, Incorporated personnel have led the design, fabrication, and flight testing of twelve unmanned aircraft and one manned aircraft. Partnered with NASA and Boeing, Area-I has developed the unmanned Prototype-Technology Evaluator and Research Aircraft or PTERA ("ptera" being Greek for wing/wing-like). The PTERA, a high-quality flight research testbed, bridges the gap between wind tunnel and manned flight testing with low-cost, low-risk flight-based evaluation of high-risk technologies. In Phase I, the PTERA was enhanced by integrating modularity and design flexibility and culminated in the design of a representative 16%-scale CRJ-700, named the PTERA-RJM for Regional Jet Model. For Phase II, the team proposes to finalize the design, fabricate, and deliver a 17ft, 278lb PTERA-RJM that is tailored for use within NASA's Aviation Safety Program to enable experiments in vehicle health monitoring, in loss of control prevention, mitigation, and recovery, in atmospheric hazard sensing and mitigation, etc.The Boeing Company supports the proposed work, as they have great interest in the PTERA platform given its following core capabilities:1) A large, low-cost airframe that minimizes scaling and Reynolds number effects, yet is easily disassembled and transported2) A modular, reconfigurable fuselage design that enables the fabrication and assembly of fuselage configurations that maintain near geometric similitude with a wide array of "tube-and-wing" aircraft using existing tooling3) Modular wing design that facilitates the integration of advanced aerodynamic treatments, split control surfaces, and aeroelastic and damage emulation mechanisms4) Integrated ballast system and movable payload/avionics racks to enable the tuning of mass/inertial properties5) Large payload capacity, voluminous payload bays, and large clamshell doors that facilitate the integration of avionics systems and provide access during flight testing

* information listed above is at the time of submission.

Agency Micro-sites


SBA logo

Department of Agriculture logo

Department of Commerce logo

Department of Defense logo

Department of Education logo

Department of Energy logo

Department of Health and Human Services logo

Department of Homeland Security logo

Department of Transportation logo

Enviromental Protection Agency logo

National Aeronautics and Space Administration logo

National Science Foundation logo
US Flag An Official Website of the United States Government