At Mach 2, is km/h higher at 15°C or −56.5°C? Why?
Is standard-atmosphere mode live weather or a reference model?
Is SR-72’s Mach 6 a measured world record or a public concept’s design target?
Why explain the X-15 and SR-71 in different categories?
What information should accompany a speed number in a citation?
Teacher / self-study answer key
Ideal dry-air model: a = √(1.4 × 287.05 × T), with T in kelvin; speed = Mach × a. At 15°C, sound speed is about 340.29 m/s and Mach 2 is about 2,450.10 km/h. At −56.5°C, these are about 295.07 m/s and 2,124.49 km/h.
15°C: warmer air has a higher local sound speed, so the same ratio gives a higher true airspeed.
A reference model, not live weather. Altitude mode uses a 6.5°C/km decrease to 11 km, then −56.5°C to 20 km.
A public concept’s design target, not a demonstrated flight record.
X-15 is a rocket research aircraft; SR-71 is an air-breathing reconnaissance jet. Propulsion, mission and record categories differ.
Aircraft/variant, source document, date, measurement or specification conditions, units and limitations. Keep event, page-update and source-check dates separate.
Fact-card answers vary by aircraft. Assess traceability and honest unknowns, rather than rewarding the largest number.