B-26/SST IN-FLIGHT SIMULATION PROGRAM,
Abstract
The simulation was flown by or demonstrated to 25 individuals, of whom 19 were subject pilots, for the purpose of comparing pilot workload involved in making ILS approaches on the frontside and backside of the thrust required curve. Approaches made on the backside of the thrust required curve simulated SST operation with fuel trimmers off, while approaches made on the frontside simulated the SST with fuel trimmers on. Airplane characteristics demonstrated were those with no stability augmentation.
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 22, 1965
- Accession Number
- AD0627792
Entities
People
- C. J. Heirich
- H. E. Worden
- R. F. Livingston
Organizations
- Lockheed Martin