In Mars Pathfinder Flight System assembly, test and launch operations (ATLO), we have completed integration of our flight "electronics box", vibrated it and spun it in a centrifuge chamber to test for launch and landing loads.
This "electronics box" is the "guts" of our three-in-one spacecraft which cruises to Mars, enters the Mars atmosphere, descends and lands, and opens up to conduct surface operations. It contains our flight computer, power conditioning and pyrotechnic firing circuits, instrument electronics, and radio.
We are currently testing it with flight software in flight-ground system tests which simulate the launch, cruise, entry/descent/landing, and surface operations mission phases. Here, we are installing its "brains". The flight system electronics will have a distinct personality after we finish this test phase in December.
Next in ATLO, we will proceed into stacking and nesting of the flight system for the string of space environmental tests planned before shipping to the launch site in August 1996.
In parallel with ATLO, we are drop testing elements of the entry/descent/landing system in various locations, qualifying its design for space use:
- Airbag drop tests in simulated Mars atmospheric pressure on a slope of rocks in the NASA Lewis Plum Brook 70-foot test chamber in Sandusky, OH
- Multi-body drop tests at a test range in Boise, ID, with a flight-like parachute, lander backshell, bridle and lander
- Flight-like cruise stage/lander backshell/bridle/lander separation tests at the China Lake Naval Research Test Facility in the Mojave desert outside of Los Angeles, where we fire live pyrotechnic devices
- Flight-like rocket drop tests, again at China Lake
- In addition, we are conducting airbag retraction and lander uprighting tests here at JPL in Pasadena.
- We are scheduled to complete the majority of our entry/descent/landing space qualifying tests in January 1996, 10 months before launch on December 2, 1996, and in time for our next NASA Formal Status Review planned for the end of January 1996.
It is evident by the nature of our test program above, that landing on the surface of a planet takes much more space qualification testing before launch--almost three times the standard set of spacecraft testing needed for launch and routine deep space flight. This is due to the additional environments associated with entry/descent/landing and surface operations mission phases.