Add to ORKGTelesat-A, which is the first of the Canadian Telesat satellites to be launched for the domestic satellite communications system is described. The launch vehicle, designated Delta-92 consists of a DSV 3p-11 extended long tank first stage with an MB-3 engine, augmented by low-drag Castor 2 solid motors. The spacecraft has a spin-stabilized electronic system powered by 23,000 solar cells, with sufficient on-board battery capability to provide full capacity power during eclipse of the solar cells. A 60-inch wide circular directional antenna which remains constantly aimed at Canada is included
Condensed technical survey for deep space monitor communications system using earth satellit
The capabilities of the Materials Engineering Branch (MEB) of the Goddard Space Flight Center, Green...
Saturn S-4B restart alternate mission launch vehicle operational flight trajectory - AS-206 vehicle ...
The STS-51 Space Shuttle Program Mission Report summarizes the payloads as well as the orbiter, exte...
Selected photographs and mission summary of Lunar Orbiter 5. The last of five Lunar Orbiter spacecra...
The three NASA/USAF lunar probes of August 17, October 13, and November 8, 1958 are described. Detai...
The configuration and functions of the ITOS D and E system are described. The system will expand the...
The STS-71 Space Shuttle Program Mission Report summarizes the Payload activities and provides detai...
This press kit for the December 1993 flight of Endeavour on Space Shuttle Mission STS-61 includes a ...
The Space Shuttle Endeavor, scheduled to launch March 2, 1995 from NASA's Kennedy Space Center, will...
The possibility of beaming power from synchronous lunar orbits (the L1 and L2 Lagrange points) to a ...
Activity conducted in the following areas is highlighted: space sciences, space transportation syste...
The STS-74 Space Shuttle Program Mission Report summarizes the Payload activities as well as the Orb...
The STS-77 Space Shuttle Program Mission Report summarizes the Payload activities as well as the: Or...
A debris/ice/thermal protection system assessment and integrated photographic analysis was conducted...
Condensed technical survey for deep space monitor communications system using earth satellit
The capabilities of the Materials Engineering Branch (MEB) of the Goddard Space Flight Center, Green...
Saturn S-4B restart alternate mission launch vehicle operational flight trajectory - AS-206 vehicle ...
The STS-51 Space Shuttle Program Mission Report summarizes the payloads as well as the orbiter, exte...
Selected photographs and mission summary of Lunar Orbiter 5. The last of five Lunar Orbiter spacecra...
The three NASA/USAF lunar probes of August 17, October 13, and November 8, 1958 are described. Detai...
The configuration and functions of the ITOS D and E system are described. The system will expand the...
The STS-71 Space Shuttle Program Mission Report summarizes the Payload activities and provides detai...
This press kit for the December 1993 flight of Endeavour on Space Shuttle Mission STS-61 includes a ...
The Space Shuttle Endeavor, scheduled to launch March 2, 1995 from NASA's Kennedy Space Center, will...
The possibility of beaming power from synchronous lunar orbits (the L1 and L2 Lagrange points) to a ...
Activity conducted in the following areas is highlighted: space sciences, space transportation syste...
The STS-74 Space Shuttle Program Mission Report summarizes the Payload activities as well as the Orb...
The STS-77 Space Shuttle Program Mission Report summarizes the Payload activities as well as the: Or...
A debris/ice/thermal protection system assessment and integrated photographic analysis was conducted...
Condensed technical survey for deep space monitor communications system using earth satellit
The capabilities of the Materials Engineering Branch (MEB) of the Goddard Space Flight Center, Green...
Saturn S-4B restart alternate mission launch vehicle operational flight trajectory - AS-206 vehicle ...