Dynamically Scaled Modular Aircraft for Flight-Based Aviation Safety Research

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX13CL58C
Agency Tracking Number: 114637
Amount: $699,962.00
Phase: Phase II
Program: SBIR
Awards Year: 2013
Solitcitation Year: 2011
Solitcitation Topic Code: A1.15
Solitcitation Number: N/A
Small Business Information
AREA-I
GA, Kennesaw, GA, 30144-3636
Duns: 829299747
Hubzone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Nicholas Alley
 Principal Investigator
 (678) 594-5227
 nalley@areai.aero
Business Contact
 Nicholas Alley
Title: Business Official
Phone: (678) 594-5227
Email: nalley@areai.aero
Research Institution
 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.

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