“YDC-3NG” Optoprime Conceptual Designs, LLC.

1. “YDC-3NG”Optoprime Conceptual Designs, LLC. Team 2 AJ Berger Colby Darlage Joshua Dias Ahmad Kamaruddin Pete Krupski Josh Mason Camrand Tucker Forward-Looking Statements This presentation contains forward-looking statements within the scope of §27 of the Securities Act of 1933, as amended, and §21E of the Securities Exchange Act of 1934, as amended, including but not limited to statements as to future operating results and plans that involve risks and uncertainties. Terminology is used that imply known and unknown risks, uncertainties, which may cause the actual results of the Company to differ materially from any forward-looking statement, expressed or implied. References to “We”, “Company” and “Optoprime” are all references to Optoprime Conceptual Designs, LLC. Investors assume all risks.

2. Isometric Views

3. Carpet Plot

4. Design Details • W/S = 100 • T/W = 0.3 • AR=8 • L = 75,000 lb • Wing t/c = 0.1 • (CL)max = 5 • C-5A Airfoil Cross-sections • (CL)max = 3.8 • Triple Slotted Krueger Internally Blown Flaps • Slats • Cruise CL = .23 • Alpha = 0 deg

5. Weight Summary • Gross Weight = 70,000 lb • Fuel Weight = 21,000 lb • Zero Fuel Weight = 51,000 lb • Max Landing Weight = 45,600 lb • Empty Weight = 23,500 lb • Wings = 4400 lb • Fuselage = 12,000 lb • Propulsion Total (incl. plumbing) = 4600 lb

6. Financial Estimates (2008 USD) • Price = $40 M • Less: • Airframe Cost = $9.8 M • Avionics Cost = $1.1 M • Engine Cost = $1.8M each (2008) • Manufacturing Cost = $14.8 • Cost of Poor Quality (COPQ) ≈ $2M • Cost of Goods Sold (per unit) = $27.5 M • Contribution Margin = $12.5 M