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Mars Pathfinder Airbag Impact Attenuation System

The Mars Pathfinder spacecraft, scheduled for launch in December 1996, is designed to validate a low cost Entry, Descent, and Landing system and to perform scientific surface operations. The Jet Propulsion Laboratory and Sandia National Laboratories teamed to design, fabricate, test and validate a prototype 0.38 scale model of an airbag impact attenuation system. A computer code was developed to predict the performance of the airbag system. A test program in Sandia's High Altitude Chamber was performed to validate the code and demonstrate the feasibility of the airbag concept and design. In addition, freefall tests were performed at representative velocities to demonstrate the structural integrity of the airbag system design. The feasibility program demonstrated that the airbag impact attenuation design will protect the lander upon impact with the Martian surface.

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LISA Pathfinder and eLISA news

Two important gatherings of the space-based gravitational-wave detector community were held in Zurich, Switzerland this past March. The first was a meeting of the Science Working Team for LISA Pathfinder (LPF), a dedicated technology demonstrator mission for a future LISA-like gravitational wave observatory. LPF is entering an extremely exciting phase with launch less than 15 months away. All flight components for both the European science payload, known as the LISA Technology Package (LTP), and the NASA science payload, known as the Space Technology 7 Disturbance Reduction System (ST7-DRS), have been delivered and are undergoing integration. The final flight component for the spacecraft bus, a cold-gas thruster based on the successful GAIA design, will be delivered later this year. Current focus is on completing integration of the science payload (see Figures 1 and 2) and preparation for operations and data analysis. After a launch in Summer 2015, LPF will take approximately 90 days to reach its operational orbit around the Earth-Sun Lagrange point (L1), where it will begin science operations. After 90 days of LTP operations followed by 90 days of DRS operations, LPF will have completed its prime mission of paving the way for a space-based observatory of gravitational waves in the milliHertz band. Immediately following the meeting of the LPF team, the eLISA consortium held its third progress meeting. The consortium (www.elisascience.org) is the organizing body of the European space-based gravitational-wave community, and it was responsible for the "The Gravitational Universe" whitepaper that resulted in the November 2013 election of a gravitational-wave science theme for ESA's Cosmic Visions L3 opportunity. In preparation for an L3 mission concept call, which is expected later this decade, and for launch in the mid 2030s, the eLISA consortium members are coordinating technology development and mission study activities which will build on the LPF results. The final mission concept is expected to include some international (non-European) contributions, and NASA has expressed an interest in participating in this ground-breaking mission. The US research community supports such a collaboration, or any other mission scenario that achieves the high-priority science of a space-based gravitational-wave observatory at the earliest possible date.

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Microbiological Cleanliness of the Mars Pathfinder Spacecraft

The recently launched Mars Pathfinder spacecraft, involving a lander and a rover scheduled to land on Mars in July 1997, was required to comply with the National Aeronautics and Space Administration planetary protection regulations for such space missions.

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Back to Mars: The Mars Pathfinder Mission

Mars Pathfinder successfully landed on the surface of Mars on July 4, 1997, and ushered in a new era in Mars exploration. This era will feature numberous low cost missions which will perform important science investigations and engage the world's population in the excitement of planetary exploration.

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Mars Pathfinder Lander Deployment Mechanisms

The Mars Pathfinder Lander will land, right itself, and open so that none of its airbag covers its solar cells. This requires two different types of mechanisms, the Airbag Retraction Actuators, and the Lander Petal Actuators which are designed for a high torque, low temperature, dirty environment, and limited life application. The development of these actuators investigated low temperature lubrication, Electrical Discharge Machining (EDM) to cut gears, and gear design for limited life use.

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Mars Pathfinder Cruise Stage/Entry Vehicle Separation Dynamics

Prior to atmospheric entry, Mars Pathfinder flight system will separate its entry vehicle from its cruise stage, and establish the entry conditions for a passive and unconventional entry, descent, and landing approach. This paper summarizes a separation dynamics analysis conducted to demonstrate that the cruise separation system design is viable and ensure that adequate design margins exist with the effects from parameter uncertainty included.

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Mars Pathfinder Project Progress Report

This paper reports on thestatus of Mars Pathfinder's drive to space qualify its flight system for launch on December 2, 1996 under a cost cap- in particular how the project is dealing with qualification fo its entry, descent and landing event and the surface operations phase as well as the normal launch and space flight phases. It also reports on its landing site selection and science plan.

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Mars Pathfinder Mission Operations Concept

Mars Pathfinder is one of the first of NASA's Discovery series of low cost planetary missions. A number of innovative design, fabrication, and management techniques have been adopted during the development phase to stay within the percent 150M (FY

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Integrated Pump Assembly - An Active Cooling System for Mars Pathfinder Thermal Control

The Mars Pathfinder spacecraft which will be launched in December 1996 features an active cooling system for controlling the temperature of the spacecraft. This will be the first time that such a mechanical pump cooling system is used on an interplanetary or long duration flight (over two weeks) in space. The major element of the cooling system is the Integrated Pump Assembly (IPA). It uses centrifugal pumps to circulate liquid Freon to transfer heat from spacecraft electronics to an external radiator. This paper describes the design, fabrication, assembly, and testing of the IPA.

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Mars Pathfinder Mission Operations Concept

Mars Pathfinder is one of NASA s new low-cost planetary missions developed to meet a $150 million cost cap. This paper describes the operations philosophy, requirements, organizational structure, and ground data system.

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Mars Pathfinder Science Investigations and Objectives

Pathfinder's primary ojective is to demonstrate an inexpensive system for curise, entry, descent, and landing on mars. Additional objective include the deployent and operation of various science instruments: a stereoscopic imager with filters on a pop up mast, and alpha proton x-ray spectometer (APXS), and an atmospheric structure instrument/meteorology package

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Using Virtual Reality for Science Mission Planning: A Mars Pathfinder Case

The Mars Pathfinder Project GDS Team has designed software that integrates virtual reality technology with existing JPL Navigational Ancillary Information Facilities (NAIF) and image processing capabilities. The result is an interactive, workstation-based application software that provides a high resolution 3-dimensional stereo display of Mars as if it were viewed through the lander camera. This paper describes the architecture and characteristics of this science mission planning software and discusses possible uses of this software by other planetary missions.

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