Pyrotechnic shock analysis and testing methods
Statistical analysis of pyrotechnic shock data from Ranger and Mariner test programs
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Statistical analysis of pyrotechnic shock data from Ranger and Mariner test programs
Space programs summary no. 37-19 - vol 6, nov 1962 to jan 1963 - space exploration programs & space sciences - dsif, ranger, mariner & voyager project
DSIF telemetry and command processing operational program for providing software to Mariner Mars 1971 mission
The requirements for marine and satellite geodesy technology are assessed with emphasis on the development of marine geodesy. Various programs and missions for identification of the satellite geodesy technology applicable to marine geodesy are analyzed along with national and international marine programs to identify the roles of satellite/marine geodesy techniques for meeting the objectives of the programs and other objectives of national interest effectively. The case for marine geodesy is developed based on the extraction of requirements documented by authoritative technical industrial people, professional geodesists, government agency personnel, and applicable technology reports.
Trapped radiation detector for Mariner C program
Space exploration programs and space science summary on Mariner, Ranger, and Surveyor projects - deep space instrumentation facility - environmental test facility
A brief overview is presented of Remotely Manned Systems with emphasis on their use as tools for exploration and operation in space. Remotely Manned Systems missions and functions in space are described and classified in relation to other existing or planned space systems. Problem areas of large-scale man-machine systems are identified based on experience in the Surveyor program, the Mariner 9 Mars orbiter project and the Apollo program. The effects of communication time delay on system performance are investigated using the average velocity of a Martian rover as performance indicator. A substantial performance increase can be achieved by providing certain autonomous capabilities to the remote system.
Generalized precision trajectory program for ranger lunar and mariner interplanetary missions
NASA space exploration programs design modifications and instrumentation developments
Mariner Mars program for 1971 and Viking project
Generalized precision trajectory program for the ranger lunar and mariner interplanetary missions
Launch to mission completion targeting techniques, computer programming for lunar and interplanetary flight programs - ranger/mariner program
Electromagnetic Interference Workshop held at JPL /Feb., 1968/ permitted an exchange of information on electromagnetic interference problems encountered in aerospace programs. The experiences related at this workshop dealt primarily with Surveyor, Lunar Orbiter, OGO, ATS, and Mariner unmanned programs.
Discussion and comparison of two data handling and control systems for the mariner interplanetary exploration programs
Space programs summary no. 37-18 - sept to nov 1962 - deep space instrumentation facility
Since Mariner, NASA-JPL planetary missions have been supported by ground software to plan and design remote sensing science observations. The software used by the science and sequence designers to plan and design observations has evolved with mission and technological advances. The original program, PEGASIS (Mariners 4, 6, and 7), was re-engineered as POGASIS (Mariner 9, Viking, and Mariner 10), and again later as POINTER (Voyager and Galileo). Each of these programs were developed under technological, political, and fiscal constraints which limited their adaptability to other missions and spacecraft designs. Implementation of a multi-mission tool, SEQ POINTER, under the auspices of the JPL Multimission Operations Systems Office (MOSO) is in progress. This version has been designed to address the limitations experienced on previous versions as they were being adapted to a new mission and spacecraft. The tool has been modularly designed with subroutine interface structures to support interchangeable celestial body and spacecraft definition models. The computational and graphics modules have also been designed to interface with data collected from previous spacecraft, or on-going observations, which describe the surface of each target body. These enhancements make SEQ POINTER a candidate for low-cost mission usage, when a remote sensing science observation design capability is required. The current and planned capabilities of the tool will be discussed. The presentation will also include a 5-10 minute video presentation demonstrating the capabilities of a proto-Cassini Project version that was adapted to test the tool. The work described in this abstract was performed by the Jet Propulsion Laboratory, California Institute of Technology, under contract to the National Aeronautics and Space Administration.
History of Mariner space program and discussion of future unmanned vehicles for exploration of interplanetary space
Launching, operation, and program development of the mariner ii spacecraft