Mars Pathfinder Microrover
The Mars Pathfinder Microrover, its operational environment and the.
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The Mars Pathfinder Microrover, its operational environment and the.
The Mars Pathfinder Microrover Flight Experiment (MFEX) is a NASA OACT flight experiment which is planned to be delivered and integrated with the Mars Pathfinder (MFP) lander and spacecraft system for landing on Mars on July 4, 1997. After landing, the MFEX rover is deployed from the lander and begins a 7 sol (1 sol=1 Martian day) mission to conduct technology experiments, deploy an alpha proton x-ray spectrometer (APXS) on rocks and soil, and image the lander as part of the engineering assessment of the mission after landing.
The Mars Pathfinder Microrover Flight Experiment (MFEX) is a NASA Office of Space Access and Technology (OSAT) flight experiment which has been delivered and integrated with the Mars Pathfinder (MPF) lander and spacecraft system. The total cost of the MFEX mission, including all subsystem design and development, test, integration with the MPF lander and operations on Mars has been capped at $25 M??is paper discusses the process and the implementation scheme which has resulted in the development of this first Mars rover.
The Microrover Flight Experiment (FEX) is a NASA Office of Space Access and Technology flight experiment of mobile vehicle technologies, whose primary mission is to determine microrover performance in the poorly understood planetary terrain of Mars.
The Mars Pathfinder Microrover Flight Experiment (MFEX) will be carried by the Mars Pathfinder mission to the surface of Mars, where it will perform technology, science and Mars mission engineeering experiments in July, 1997.
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This paper provides an overview of the design of the Mars Pathfinder Microrover with an emphasis on how its integrated design enables it to perform all of the functions normally associated with entire spacecraft. The impact that mass, volume, and power constraints have had upon the design will also be discussed.
A discussion of the power requirements for the Mars Pathfinder Mission is given. Topics include: battery requirements; cell design; battery design; test descriptions and results. A summary of the results is also included.
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The NASA Lewis Research Center has a prime role in the Mars Pathfinder mission, the first in the series of Discovery-class missions, sponsored by NASA Headquarter's Office of Space Science. Mars Pathfinder is an engineering proof-of-concept mission intended to demonstrate the successful deployment of scientific instruments, including a small rover, on a planetary body and to gain engineering design information for follow-on systems. The mission was launched in December 1996 and will land on Mars on July 4, 1997.
The Microrover Flight Experiment (MFEX) is a NSAS OACT (Office of Advanced Concepts and Technology) flight experiment which, integrated with the Mars Pathfinder (MPF) lander and spacecraft system, landed on Mars on July 4, 1997.
The Microrover Flight Experiment (MFEX) is a NASA OACT flight experiment which is planned to be delivered and integrated with the Mars Pathfinder (MPF) lander and spacecraft system for landing on Mars on July 4, 1997.
The Microrover Flight Experiment (MFEX) is a NASA Office of Space Access and Technology flight experiment of mobile vehicle technologies, whose primary mission is to determine microrover performance in the poorly understood planetary terrain of Mars.
Explore the source record for details and available documents.
Explore the source record for details and available documents.
The advent of spacecraft miniaturization promises a new generation of affordable planetary missions; they will be more cost effective - by one to two orders of magniture - than those of traditional design.
On-board the Mars Pathfinder spacecraft, launched in December of 1996, is a small roving vehicle named Sojourner. On Sojourner is an experiment to determine the abrasive characteristics of the Martian surface, called the Wheel Abrasion Experiment (WAE). The experiment works as follows: one of the wheels of the rover has a strip of black anodized aluminum bonded to the tread. The aluminum strip has thin coatings of aluminum, nickel and platinum deposited in patches. There are five (5) patches or samples of each metal, and the patches range in thickness from 200 A to 1000 A. The different metals were chosen for their differing hardness and their environmental stability. As the wheel is spun in the Martian soil, the thin patches of metal are abraded away, exposing the black anodization. The abrasion is monitored by measuring the amount of light reflected off of the samples. A photodetector was developed for this purpose, and that is the subject of this paper.
The Mars Pathfinder Project plans a December 1996 launch of a single spacecraft.