About this document
Concorde Performance Calculations by Shiva Yadav is a document available to read on EtoBox.
1) The maximum velocity at sea level for the aircraft is approximately 1250 feet/second. 2) The climb rate at sea level decreases as airspeed increases, reaching 0 feet/minute at around 1300-1500 feet/second. 3) The approximate glide angle is 8 degrees, and the glide range at a cruise altitude of 60,000 feet is 454794 feet.
- Author
- Shiva Yadav
- Language
- EN