Beschreibung : The mission was a four-hour, two-orbit test of the Orion crew module featuring a high apogee on the second orbit and concluding with a high-energy reentry at around 20,000 miles per hour (32,000 km/h; 8,900 m/s). This mission design corresponds to the Apollo 4 mission of 1967, which validated the Apollo flight control system and heat shield at re-entry conditions planned for the return from lunar missions.
Cape Canaveral post stamp.

USA 3042 - picture enhanced ?

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ORION · EXPLORATION FLIGHT TEST-1 EFT-1 · DELTA IV HEAVY ROCKET