The LANDSAT-1 spacecraft was launched from the Western Test Range on 23 July 1972, at 18:08:06.508Z. The launch and orbital injection phase of the space flight was nominal and deployment of the spacecraft followed predictions. Orbital operations of the spacecraft and payload subsystems were satisfactory through Orbit 147, after which an internal short circuit disabled one of the Wideband Video Tape Recorders (WBVTR-2). Operations resumed until Orbit 196, when the Return Beam Vidicon failed to respond when commanded off. The RBV was commanded off via alternate commands. LANDSAT-1 continued to perform its imaging mission with the Multispectral Scanner and the remaining Wideband Video Tape Recorder providing image data
Investigation of cost effective utilization of space maintenance and repair techniques to despin App...
The results are presented of the mission analysis performed by Computer Sciences Corporation (CSC) i...
Iterative procedures were used to analyze the performance of two preliminary shuttle/GPS navigation ...
The LANDSAT operations from launch through orbital instrument observations are reviewed. Orbital par...
The LANDSAT-1 spacecraft was launched from the Western Test Range on 23 July 1972, at 18:08:06.508Z....
A flight performance analysis of the LANDSAT-1 spacecraft is presented, and some of the following we...
Flight performances of LANDSAT 1 and LANDSAT 2 are evaluated. The in-flight systems discussed are: ...
The orbital operations and payload subsystems performance of LANDSAT 1 and LANDSAT 2 are described. ...
The performance of satellite subsystems and the response of in-orbit payload systems are summarized....
The flight performance of Landsat 1 and Landsat 2 is analyzed. Flight operations of the satellites a...
LANDSAT 1 and 2 operations were described, giving detailed charts and tables of their performances s...
The activities and progress in the satellite tracking and earth dynamics research during the first h...
Flight performance analysis of LANDSAT 2 and LANDSAT 3 are presented for the period July 1978 to Oct...
The spaceborne testing equipment carried by the orbiter and the measuring equipment onboard the sate...
During 1971, a series of very long baseline interferometer observations were made of the C-band (6 c...
Investigation of cost effective utilization of space maintenance and repair techniques to despin App...
The results are presented of the mission analysis performed by Computer Sciences Corporation (CSC) i...
Iterative procedures were used to analyze the performance of two preliminary shuttle/GPS navigation ...
The LANDSAT operations from launch through orbital instrument observations are reviewed. Orbital par...
The LANDSAT-1 spacecraft was launched from the Western Test Range on 23 July 1972, at 18:08:06.508Z....
A flight performance analysis of the LANDSAT-1 spacecraft is presented, and some of the following we...
Flight performances of LANDSAT 1 and LANDSAT 2 are evaluated. The in-flight systems discussed are: ...
The orbital operations and payload subsystems performance of LANDSAT 1 and LANDSAT 2 are described. ...
The performance of satellite subsystems and the response of in-orbit payload systems are summarized....
The flight performance of Landsat 1 and Landsat 2 is analyzed. Flight operations of the satellites a...
LANDSAT 1 and 2 operations were described, giving detailed charts and tables of their performances s...
The activities and progress in the satellite tracking and earth dynamics research during the first h...
Flight performance analysis of LANDSAT 2 and LANDSAT 3 are presented for the period July 1978 to Oct...
The spaceborne testing equipment carried by the orbiter and the measuring equipment onboard the sate...
During 1971, a series of very long baseline interferometer observations were made of the C-band (6 c...
Investigation of cost effective utilization of space maintenance and repair techniques to despin App...
The results are presented of the mission analysis performed by Computer Sciences Corporation (CSC) i...
Iterative procedures were used to analyze the performance of two preliminary shuttle/GPS navigation ...