Explorer 41 (IMP-G)

Launch Success

Liftoff Time (GMT)

08:47:58

Saturday June 21, 1969

Mission Details

Explorer 41 (IMP-G)

Wiki

Explorer 41 (IMP-G) was a spin-stabilized spacecraft placed into a high-inclination, highly elliptic orbit to measure energetic particles, magnetic fields, and plasma in cislunar space. The line of apsides and the satellite spin vector were within a few degrees of being parallel and normal, respectively, to the ecliptic plane. Initial local time of apogee was about 1300 h. Initial satellite spin rate was 27.5 rpm. The basic telemetry sequence was 20.48 s. The spacecraft functioned very well from launch until it decayed from orbit on December 23, 1972. Data transmission was nearly 100% for the spacecraft life except for the interval from November 15, 1971, to February 1, 1972, when data acquisition was limited to the vicinity of the magnetotail neutral sheet.

Highly Elliptical Orbit

1 Payload

175 kilograms

Rocket

Retired
Delta E1

Active 1966 to 1971


Payload to Orbit

GTO: 205 kg

Stages

3

Strap-ons

3

Launch Site

SLC-2W

Vandenberg SFB, California, USA

Fastest Turnaround

13 days 1 hour

Stats

Delta E


22nd

Mission

3rd

Mission of 1969

1969


61st

Orbital launch attempt