Pad LC-19 ()
| Altitude: 320km x 160.3km
Inclination: xxx degrees
Duration: 4 Days, hours, min, seconds
Demonstrate GLV performance; flight qualify subsystems, Determine exit heating of GLV and spacecraft. Demonstrate structural integrity of GLV and spacecraft; Demonstrate GLV and ground guidance systems performance in achieving proper orbital insertion; Monitor, evaluate GLV switchover circuits.
Secondary Objectives included: Evaluate operational procedures for GLV trajectory and cutoff conditions; Verify orbital insertion by tracking C-band transponder in spacecraft; Demonstrate performance of launch and tracking networks; Provide training for flight controllers and prelaunch and launch crews and facilities.
| April 8, 1964 11:00:01.69 am EST.
|| April 12, 1964
Successful orbital test of the Titan-II launch vehicle, spacecraft structural integrity and launch vehicle spacecraft compatibility. Unmanned, no plan to recover. Mission terminated after 3 orbits and spacecraft disintegrated 3.5 days after launch). All primary and secondary