Please make a donation to support Gunter's Space Page.
Thank you very much for visiting Gunter's Space Page. I hope that this site is useful and informative for you.
If you appreciate the information provided on this site, please consider supporting my work by making a simple and secure donation via PayPal. Please help to run the website and keep everything free of charge. Thank you very much.

Transit-5E 3 (S/N 41 ?)

Transit-5E 3 [JHU/APL]

Three Transit-5B series satellites were launched by Thor-DSV2A Able-Star rockets with piggyback Transit-5E series research satellites. The 5E series were launched to obtain environmental data in the vicinity of the operational orbit of Transit satellites and used solar power. The Transit-5Es, which reached orbit, yielded excelent data.

This series was built on Transit busses based on the Transit 5A series.

Transit-5E 3 featured following systems:

  • Two oven-controlled oscillators (9 parts in 1011 and 7 parts in 1011)
  • Transmitters: 54, 162, 324, and 648 MHz
  • Transistor beta experiment
  • Transistor leakage experiment
  • Magnetic stabilization system
  • Power system: Solar cells Ni-Cd batteries and DC/DC converter
  • Solar charge limiter
  • Automatic temperature control
  • Command system: 48 possible operating modes
  • Telemetry system: 35 channel reed relay commutator and 35 channel solid state commutator
  • Whip and dipole antenna system

The objectives of Transit-5E 3 were:

  1. Evaluate the effect on the operational system of refraction on radio signal propagation.
  2. Test an experimental solid-state telemetry commutator.
  3. Obtain flight test experience of battery-charge control by current limiting, since charge control circuitry was intended for use in future satellites.

Objective No. 4 was partially achieved in that charge control design information gained aboard 5E-3 was used to improve charge control circuitry in future navigation satellites. However, improper charge control circuit operation aboard 5E-3 permitted only partial realization of Objective No. 1 and ultimately precluded attainment of Objective No. 2. Objective No. 3 was met.

The charge control circuit malfunction demanded continuous adjustment of satellite loads to avoid the development of serious thermal troubles as well as to determine the inter-relationship of the parameters which assisted in the analysis of the problem. Because of this continual adjustment, good four-frequency data which are mandatory for proper ionospheric research were not obtained over extended periods of time.

The experimental solid state commutator performed perfectly, and was the prototype for those used in subsequent APL satellites. 5E-3 transmissions were last received 19 July 1964.

Nation: USA
Type / Application: Experimental
Operator: USN
Contractors: Johns Hopkins University Applied Physics Laboratory (APL)
Equipment: ?
Configuration: Transit-Bus
Propulsion: ?
Power: 4 deployable solar arrays, batteries
Mass: 52 kg
Orbit: 1078 km × 1108 km, 90.0
Satellite COSPAR Date LS Launch Vehicle Remarks
Transit-5E 3 (S/N 41 ?) 1963-049C 05.12.1963 Va 75-1-1 Thor-DSV2A Able-Star with Transit-5BN 2

Cite this page: