Viking '75 Science Test Lander, Detail photographs of the Science Test Lander from Viking '75 |
Viking '75 Science Test Lander, Detail photographs of the Science Test Lander from Viking '75 |
May 16 2012, 03:59 AM
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Member Group: Members Posts: 101 Joined: 3-May 12 From: Massachusetts, USA Member No.: 6392 |
Recently I spent an enjoyable afternoon photographing the Viking '75 Mars Lander
which is on display at the Virginia Air and Space Center in Hampton VA. Based on many details, I am sure this is the so-called Science Test Lander (STL) which was installed in the NASA/JPL "sandbox" during the missions. I have uploaded 277 detail photos (totaling nearly 2GB) to a Picasa Web album. (As far as I know, the best/only way to download them all is to install and execute Google's free Picasa application for Windows PCs. Note a quirk with the Picasa Web magnifier tool: on large images such as these, the full resolution usually is not loaded right away when you activate the magnifier. If you wait ten seconds or so, usually the full 4K-pixel version will become available via the navigator pop-up in the corner. Sometimes it never does, however.) The STL in its current museum display configuration has two very interesting attributes. First, the insulation blankets and cloth covers which normally surround the fuel tanks, associated plumbing, and roll-control thrusters has been removed. I happily captured a fair number of photos of the exposed (and complex!) fuel-system plumbing, valves, wiring, and thrusters. Second, the lander's bottom cover plate has been cut open in the 30-inch square area normally covered by the Terminal Descent Landing Radar (TDLR) box. The TDLR is not installed; instead it is mocked-up on two side with tall white flanges. I would like to see an accurate TDLR someday (the Smithsonian's Proof Test Capsule is also missing a TDLR), so it's a bit of a shame not to find one here. However, the trade-off is wonderful -- the large opening in the bottom allows a peek at the lander's interior! It is not really possible to see visually inside, due to geometry of the museum display, but a carefully-positioned camera can get some views. :-) The STL body is essentially empty, but a few interesting details are present. The dacron-covered insulation blankets lining the interior sidebeam walls are there, restrained with authentic vertical nylon ties. The Equipment Plate is installed, which is a large hexagonal aluminum plate spanning the interior about five inches down from the lander's top cover plate. (The computer, batteries, science instruments, radios, etc. were bolted to and hung from the bottom of the Equipment Plate.) The plate is partially painted black (for thermal control) in areas which were not to be covered by mounted components, and this is visible. The thin coolant-loop tubing which snakes around the underside of the Equipment Plate is there. The three cylindrical struts from which the TDLR was to be hung are there. The Thermal Switches to which the Radioisotope Thermoelectric Generators were mounted are there, and I managed to capture a peek at the flexible copper "Contactor" of one of them. The STL has somewhat simplified external wiring, and the externally-mounted electronics units on sides 1 and 3 are simple wood mock-ups. This includes the Inertial Reference Unit, the two Radar Altimeter Electronics units, and the Valve Drive Amplifier. The three Terminal Descent Engines are also mostly wood mock-ups, however TDE #2 (on the "front") has an authentic top plate and gold thermal shield. I was able to take a number of detail measurements, which will eventually be incorporated into plans I've barely begun to create. All in all, I was very happy to have made the trip to see this lander. -- Tom |
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Jan 12 2013, 03:35 AM
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Member Group: Members Posts: 101 Joined: 3-May 12 From: Massachusetts, USA Member No.: 6392 |
I recently discovered some new (to me) information about the origin of the Viking lander known as the "Science Test Lander" (STL). There is an article titled Viking That Will Never Fly in the August 11 1975 issue of the Langley Researcher newsletter. Accompanying the article is a photograph (reproduced below) of the STL with the caption:
QUOTE Engineers Leonard V. Clark of VPO (Viking Project Office) and Vernon P. Gillespie of SED (System Engineering Division) discuss the status of the Viking Science Test Lander being fabricated by personnel of SED and FID (Flight Instrumentation Divisions). This full-scale working model of the Viking Lander will be shipped to JPL (Jet Propulsion Laboratory) in Pasadena, California, in late August for utilization during Viking Flight Operations. The article essentially confirms in my mind that the circa-1975 STL is a distinct unit from the Proof Test Capsule (now in the Smithsonian National Air and Space Museum) which was assembled earlier by Martin Marietta in Denver and used extensively in numerous test programs during lander development. The full text of the article reads as follows: QUOTE Viking That Will Never Fly Not all the Viking Landers will see the light or life on Mars. While its two sisters mated with Orbiters, speed to Mars, the third capsule will sit complacently here on Earth, content to be viewed and tested as a working model. The third Viking Lander is called the Science Test Lander (STL). It is a full-scale model that will be used during the period of Flight Operations at Jet Propulsion Laboratory (JPL) in Pasadena, California. The STL is an exact duplicate in appearance and geometry of the Flight Landers. A particular emphasis has been placed on fidelity of the top deck of the Lander where the Mars surface sample inlets to the principle science instruments (biology, GCMS (Gas Chromatograph/Mass Spectrometer) and XRFS (X-ray Fluorescence Spectrometer) are located. An important feature of the Lander model is its operational subsystems, namely, a pair of facsimile cameras and a surface sampler. The cameras will be operated to scan 360 degrees to take panoramic pictures of the area around the Lander. They can be used in a special "line scanning" mode to detect motions. Its color filters can perform chemical minerology investigations on the surface near the Lander. The surface sampler can be commanded to reach out its retractable ten foot arm, scoop up the Mars surface samples and deposit the grains into the mini-laboratories that will perform the experiments. The model has been assembled at Langley using an assortment of surplus hardware from the many test programs that preceded the building of the flight Lander components. The STL will be shipped to JPL in late August. It will be installed by Langley staff in the Atrium adjacent to Von Karman Auditorium. The Atrium, enclosed by floor to ceiling glass viewing windows, was reconstructed and powered to house the working model in a suitable surrounding. The facility will be operational by October. The Surface Sampler Team of the Viking Science Group is responsible for the operational phase. By testing and studying this working capsule, the crew will be able to understand, command and control the other two Landers for their performance and data return. The facility will initially be used to provide camera and surface sampler data for the Lander Simulation System, and to support Flight Team Test and Training exercises. Later, the STL will be used extensively by the Imaging and Surface Sampler Teams to develop an instrument performance data base, to develop command sequences for nominal and off-nominal situations, and to develop and verify flight commands. Sometimes called the "Kiwi" or "Gooni Bird" by the joking staff, who nonetheless are proud to be its guardian, the STL will provide an interesting close-up display during its working hours to the fascinated viewers. Edited to add some more information: I was re-reading a set of Viking Mission Status Bulletins that I acquired a while ago, and came across a definitive statement in the cover story of No. 36, about Lander 1's early surface sampler locking-pin troubles. The story includes the following statement clearly indicating the independent status of the STL and PTC: QUOTE The situation was quickly evaluated, and tests were made to duplicate and determine the nature of the problem using the science test Lander at JPL and the proof test Lander at Martin Marietta in Denver. |
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