Launch launch vehicle lifts Gemini 4 into orbit, June 3, 1965. Launched from
LC-19 at
Cape Kennedy Air Force Station,
Florida, Gemini 4 was the first flight to be controlled by the new
Mission Control Center at the
Manned Spacecraft Center in
Houston, Texas, which had to conduct three-shift operations due to the flight's long duration. The broadcast of the launch was itself historic. For the first time an international audience, from 12 European nations, could watch the lift-off on live
television via the
Early Bird satellite.
Press interest, due to the satellite broadcast and the new center in Houston, proved to be so high that NASA had to lease buildings to accommodate the 1,100 print and broadcast journalists who requested accreditation. Flight control shifted from Cape Kennedy to Houston as soon as the vehicle cleared the launch tower. At liftoff, two roll transients caused by misalignment of the Titan first-stage engines occurred; these were quickly corrected by the autopilot. The fuel top-off umbilical failed to detach and was pulled loose when the booster had climbed about . A small oscillation in the pitch and yaw planes resulted from this. Performance of all launch vehicle systems was nearly nominal. Some modifications had been made to the guidance program on Gemini 4's booster to produce a less lofted flight trajectory and a lower altitude at
booster engine cut-off (BECO) than on Gemini 3; these were generally successful despite a still somewhat lofted flight path. BECO occurred at T+152 seconds; second-stage engine cut-off (SECO) occurred at T+333 seconds. The spacecraft entered into an orbit.
Rendezvous attempt On the first orbit, McDivitt attempted to
rendezvous with the spent Titan second stage. This was unsuccessful for a number of reasons: • NASA engineers had not yet worked out the idiosyncrasies of
orbital mechanics involved in rendezvous, which are counter-intuitive. Simply thrusting the spacecraft toward the target changed its orbital altitude and velocity relative to the target. When McDivitt tried this, he found himself moving away and downward, as the retrograde thrust lowered his orbit, increasing his speed. • The stage was dumping its residual propellant, causing it to move around in various directions relative to the Gemini. They powered down the spacecraft's maneuvering system, intending to drift for the next two-and-a-half days to conserve the remaining fuel. They also intended to sleep alternate four-hour periods, but this turned out to be extremely difficult with the constant radio communications and the small cabin, about the size of the front seats of a
compact car. White's 20-minute space walk was the mission's highlight, with McDivitt's photographs being published worldwide. These also showed White wearing an
Omega Speedmaster chronograph watch on his spacesuit sleeve, one of two makes which had been approved by NASA for space use following extensive tests. Omega were unaware of these tests or the fact that its product was going to be used in space, until the photos. The model worn during the spacewalk is now known as the "Ed White" by watch collectors.
Experiments Eleven
experiments were carried on the
spacecraft: As they lacked any means of measuring water intake, they attempted to minimize consumption of it and also reported high amounts of gas bubbles in the water from the water dispenser. They experienced a degree of eye, nose, and throat irritation early in the flight and post-landing. This was attributed to ammonia fumes from the flame retardant used in the cabin, which was changed to a different material on subsequent flights.
Reentry by telephone aboard the aircraft carrier USS
Wasp The computer failed on the 48th revolution when McDivitt tried to update it for reentry. It would not turn off and eventually stopped working altogether. This was unfortunate for
IBM, which had just put an advertisement suggesting that its computers were so reliable that even NASA used them.{{cite web Reentry came on the 62nd revolution. An open-loop rolling reentry (as used in Mercury) had to be used because of the computer failure. The astronauts began rolling the spacecraft at altitude to increase its stability. They started slowing the roll rate at and stopped it by . The
drogue parachute deployed shortly after this, and the main deployed at . A malfunctioning thruster caused the roll to be much faster than planned, and the landing was rough. Despite the rough landing, neither of the crew encountered any problems, contrary to NASA doctors' concerns about their landing upright as opposed to on their backs, as in Mercury after four days in space. Even though they landed short of the intended landing target, some ships had already started steaming to the touchdown point, and a helicopter was able to see them land. The prime recovery ship was . The recovery was supported by 10,249 U.S. Department of Defense personnel, 134 aircraft, and 26 ships. Postflight medical examination found the astronauts to be in good health, and no significant physiological changes were found. ==Insignia==