Project FIRE (Flight Investigation Reentry Environment) was a United States NASA effort to determine the effects of atmospheric entry on spacecraft materials.[1] [2]
Project FIRE used both ground testing in wind tunnels and flight tests to test the effects of reentry heating on spacecraft materials, using a subscale model of the Apollo Command Module.
Wind tunnel testing occurred at the 4-foot Unitary Plan Wind Tunnel, the High-Temperature Tunnel, and the Thermal Structures Tunnel at the Langley Research Center located in Hampton, Virginia.
Recoverable reentry packages were flight tested using Atlas-D rockets with Antares-2 solid fuel upperstages (used on the Scout rocket family),[3] [4] launched from LC 12 at Cape Canaveral Air Force Station in Florida, United States.[5]
The first Project FIRE reentry package was propelled to an altitude of 122km (76miles) by an Atlas-D Antares-2 launch vehicle (missile 263D) on 14 April 1964.[6]
Following a coasting phase that reached an apogee exceeding 800km (500miles) the velocity package initiated the reentry vehicle's trajectory, plunging it into a trajectory at a velocity of 11300m/s with a minus 15 degree trajectory. As the spacecraft descended towards Earth, a solid-fuel Antares II rocket positioned behind the payload ignited for 30 seconds, elevating the descent speed to 40501km/h. Temperature data from the spacecraft's instruments were transmitted to the ground, indicating an estimated exterior temperature of 11400K.
Approximately 32 minutes post-launch, the spacecraft made impact into the Atlantic Ocean.
During the second trial, a propelled instrumented probe, referred to as a "flying thermometer," was launched into a ballistic trajectory over 805km (500miles) high by an Atlas-D Antares-2 booster (missile 264D) on 22 May 1965.
As the spacecraft initiated its descent after 26 minutes of flight, the Antares II rocket accelerated its fall. The probe entered the atmosphere at a velocity of 40877km/h, generating temperatures of approximately 11206K. Ground stations received data on heating throughout the descent.
Thirty-two minutes post-launch, and a mere six minutes after the Antares ignition, the device impacted in the Atlantic Ocean approximately 8256km (5,130miles) southeast of the Cape.