HE-161 LAP-C
3,491 UltravioletBlood
11 days ago
Auto Credit Based on UltravioletBlood's HE-161 LAP-B
Third iteration of the light weapon testing platform. The propeller engine was replaced with the HE JS-200 Turbojet engine. Along with the slightly increased wing area and more sturdy landing gear, this allows for bigger and heavier payloads. Lateral stability was also improved.
AG1 activates pitch stabiliser
Free to use for weapon testing
Specifications
Spotlights
- DISHWASHER2005 8 days ago
- AManWillDieButNotHisIdeas 11 days ago
- MizeaO 10 days ago
General Characteristics
- Predecessor HE-161 LAP-B
- Created On Windows
- Wingspan 39.7ft (12.1m)
- Length 24.0ft (7.3m)
- Height 9.8ft (3.0m)
- Empty Weight 4,339lbs (1,968kg)
- Loaded Weight 5,721lbs (2,595kg)
Performance
- Power/Weight Ratio 0.824
- Wing Loading 26.6lbs/ft2 (129.8kg/m2)
- Wing Area 215.2ft2 (20.0m2)
- Drag Points 1359
Parts
- Number of Parts 103
- Control Surfaces 6
- Performance Cost 559