The Rochett Spear G1 Delta is an air superiority and multirole, single-engine, delta wing, fourth-generation
fighter aircraft that was manufactured by Rochett Aerial Industries. It was designed in mid 1976 as part of the Spear G1 series of military aircraft that was to replace the aging Rochett Epsilon and Blockets JF-5 multirole aircraft that was introduced twenty five years earlier in the Block Air Force and Navy.
The aircraft is based on the design of the French Dassault Mirage 2000.
ACTIVATION GUIDE
AG-1 = J & K-Raider missiles
AG-2 = Drop Tanks
AG-3 = Afterburner
AG-4 = Parachute
Specifications
General Characteristics
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- Wingspan 21.7ft (6.6m)
- Length 37.5ft (11.4m)
- Height 10.3ft (3.1m)
- Empty Weight N/A
- Loaded Weight 11,911lbs (5,402kg)
Performance
- Power/Weight Ratio 13.678
- Wing Loading 23.9lbs/ft2 (116.9kg/m2)
- Wing Area 497.6ft2 (46.2m2)
- Drag Points 1118
Parts
- Number of Parts 173
- Control Surfaces 10
- Performance Cost 813
