Explorer 49


Explorer 49 was a satellite launched on June 10, 1973 for long wave radio astronomy research. It had four X-shaped antenna elements, which made it one of the largest spacecraft ever built.

Launch

Explorer 49 was launched after the termination of the Apollo program, and although it did not examine the Moon directly, it became the last American lunar orbital mission until the launch of Clementine spacecraft in 1994.
It was launched on June 10, 1973, 14:13:00 UTC in the Rocket Delta 1913 from the Launch site Cape Canaveral LC-17B.

Orbit

This mission was the second of a pair of Radio Astronomy Explorer satellites, Explorer 38 or RAE-A being the first. Explorer 49 was placed into lunar orbit to provide radio astronomical measurements of the planets, the Sun, and the galaxy over the frequency range of 25 kHz to 13.1 MHz. Since the spacecraft's design used gravity gradient booms, the lumpy lunar gravity field was a problem for the mission scientists.

Mission

Explorer 49 was placed in lunar orbit to record radio measurements from 25 kHz to 13.1 MHz of the Milky Way galaxy. Explorer 49 was placed in to lunar orbit so that radio waves from Earth would not be as big of an interference as Explorer 38 had discovered.

Experiments

The principal investigator for all the experiments was Dr. Robert G. Stone.
  1. Step Frequency Radiometers: Explorer 49 was equipped with two Ryle-Vonberg receivers one on the upper V-antenna and the other on the lower V-antenna.The radiometers were designed to measure at nine frequencies from.45 to 9.18 MHz.
  2. Rapid-Burst Receivers: Explorer 49 had three rapid burst receivers, one on the upper V-antenna one the lower V-antenna and the third on the middle dipole antenna. The Burst Receivers were composed of a pair of IF Amplifiers and detectors one of the pair was used for back up. They detected on 32 channels between 25 kHz and 13.1 MHz.
  3. Impedance Probe: This was to test the engineering to calibrate the upper V-antenna.

    Data

Data were returned to Earth via either a low power UHF/ transmitter, in real time, or stored in an on board tape recorder and transmitted to Earth via a high power UHF transmitter. Two tape recorders provided backup storage.

Defects

The third burst receiver on the dipole antenna failed after the first week and no data resulted from the receiver.
A mechanical flaw in the lower V-antenna caused the leg to only deploy to a length of instead of. This was corrected in November 1974 and the leg extended to the full intended length.