Explorer 50 (IMP-J)

Launch Success

Liftoff Time (GMT)

02:26:00

Friday October 26, 1973

Watch Replay

24/7 Coverage

Mission Details

Explorer 50 (IMP-J)

Wiki

IMP 8 (Explorer 50), the last satellite of the IMP series, was a drum-shaped spacecraft, 135.6 cm across and 157.4 cm high, instrumented for interplanetary and magnetotail studies of cosmic rays, energetic solar particles, plasma, and electric and magnetic fields. Its initial orbit was more elliptical than intended, with apogee and perigee distances of about 45 and 25 earth radii. Its eccentricity decreased after launch. Its orbital inclination varied between 0 deg and about 55 deg with a periodicity of several years. The spacecraft spin axis was normal to the ecliptic plane, and the spin rate was 23 rpm. The data telemetry rate was 1600 bps. The spacecraft was in the solar wind for 7 to 8 days of every 12.5 day orbit. Telemetry coverage was 90% in the early years, but only 60-70% through most of the 1980's and early 1990's. Coverage returned to the 90% range in the mid to late 1990's. The objectives of the extended IMP-8 operations were to provide solar wind parameters as input for magnetospheric studies and as a 1-AU baseline for deep space studies, and to continue solar cycle variation studies with a single set of well-calibrated and understood instruments. In October, 2001, IMP 8 was terminated as an independent mission. Telemetry acquisition resumed after about three months at Canberra only (30-50% coverage), as an adjunct to the Voyager and Ulysses missions. The last useful science data from IMP 8 was acquired on 07 October 2006.

Highly Elliptical Orbit

1 Payload

371 kilograms

Rocket

Retired
Delta 1604

Active 1972 to 1973


Stages

3

Strap-ons

6

Launch Site

SLC-17B

Cape Canaveral SFS, Florida, USA

Fastest Turnaround

20 days 2 hours

Stats

Delta 1000 Series


5th

Mission

3rd

Mission of 1973

1973


85th

Orbital launch attempt