Design project: Viper

Abstract

Verbatim from NASA NTRS. Not paraphrased, not summarized.

The design specification of the primary flight trainer are: must conform to F.A.R. 23, including the crashworthiness standards; is limited to two to four occupants; engine must be FAA certified; must comply with FAA standards for VFR and allow for upgrade to IFR flights; must be at least utility category with good spin recovery characteristics; must have a structural lifetime of at least 10,000 flight hours; capable of either of two training missions: climb to 5,000 ft., cruise 500 Nm. plus reserve, land, or climb to 1,000 ft. and descend ten cycles for landing practice, climb to 3,000 ft., maneuver at two g's for 15 minutes, cruise 100 Nm. and land; must have a cruise speed of at least 120 knots; must take-off or land on a runway no longer than 3,000 ft; and has a cost goal of $50,000, not including avionics, for production of 1,000 airplanes over a five year period.

Authors

• Haithcock, Stephen Embry-Riddle Aeronautical Univ.
• Koncak, Kyle Embry-Riddle Aeronautical Univ.
• Neufang, Rich Embry-Riddle Aeronautical Univ.
• Paufler, David Embry-Riddle Aeronautical Univ.
• Snow, Russ Embry-Riddle Aeronautical Univ.
• Wlad, Frank Embry-Riddle Aeronautical Univ.