Foam impact centered on panel 6 of wing's edge
BY WILLIAM HARWOOD
STORY WRITTEN FOR CBS NEWS "SPACE PLACE" & USED WITH PERMISSION
Posted: March 26, 2003
Engineers hope to begin analyzing data this weekend from a recovered tape recorder that stored readings from some 721 sensors throughout the shuttle Columbia during its final 45 minutes of flight. Analysts hope the data will help them precisely map out the flow of hot gas through the doomed ship's left wing to confirm and refine - or possibly modify - current theories about where the initial breach occurred and how the deadly plume then worked its way through the interior of the wing.
"In a perfect world, we will have 721 measurements, sensor outputs," said Scott Hubbard, a member of the Columbia Accident Investigation Board. "This covers the wings, the fuselage and the vertical tail surfaces. Of particular interest are going to be 182 pressure measurements, 53 temperature measurements and 447 loads, dynamics and stress measurements.
"Among these will include a series of measurements - if we get all the data back - on the left wing: strains, stresses and strains, temperature and pressures.
"Now we have to note, this has been through a very severe environment," he cautioned. "We don't know if the tape has been demagnetized, we don't know yet the quality of the data in there."
But if the tape is, in fact, readable, "this would be a gold mine of information that could lead us to a much, much better understanding of what happened throughout the vehicle and particularly on the left wing."
During a news conference following a public hearing by the CAIB, Hubbard said additional study of enhanced photography of foam debris slamming into Columbia's left wing shows the material hit the underside of the ship's leading edge in a roughly two-square-foot region centered on a specific panel of protective carbon composite material just forward of the left main landing gear wheel well.
The two independent lines of evidence are consistent with a breach at or near reinforced carbon carbon - RCC - panel No. 6, or an adjacent closeout panel, that allowed a deadly plume of superheated air to burn its way into the wing, triggering a catastrophic chain of events that led to Columbia's destruction 200,000 feet above Texas.
At today's hearing, two CAIB investigators revealed yet another piece of evidence that supports a burn through near the suspected foam impact point at RCC-6: A partially melted RCC support strut from just behind RCC panel 11, located outboard of RCC-6, that shows hot gas in a cavity enclosed by the wing's RCC panels was moving outboard, as one would expect from a breach located closer inboard to the fuselage.
"There's actually an open space inside the leading edge," said Gregory Kovacs, a professor at Stanford University. "So it's possible if there was a breach, something could have flowed down that open space and then eroded the components in there. So on that score, I think we are thinking about flows down there, where they're concentrated maybe closer to the breach. That's the kind of thinking we're going through."
As it turns out, two temperature sensors monitored by the OEX recorder were mounted underneath insulation on the wing spar behind RCC panels 9 and 10. If a breach really did occur inboard of there, near RCC-6, for example, those sensors may have recorded the initial intrusion of hot gas before it ate its way into the interior of the wing.
"It's expected that if this was a normal mission, (the OEX recorder) would have about 30 minutes of data from ascent and in a nominal mission, an hour of entry data," Hubbard said.
But Columbia's re-entry ended 45 minutes after it began. In addition, the wiring from many sensors in the left wing was routed around the left main landing gear wheel well. Many of those wires may have been severed by the super-heated plume that ultimately burned its way into the wheel well. Even so, that would not affect data from other sensors expected to shed light on the thermal environment and the aerodynamic forces acting on the ship in its final moments.
To put all of that in perspective, here is a brief recap of what investigators believe may have happened to Columbia:
"We have focused a lot of our attention on the left wing and particularly the left wing leading edge," Hubbard said. "If the sensors that are there were active and working and got recorded, that information would be extremely valuable. If for some reason those sensors dropped out, the orientation of the vehicle, from some of the other sensors that also help us determine the attitude of the vehicle, might give us a better sense of what was going on."
Starting around April 6, engineers at the Southwest Research Institute in San Antonio, Texas, plan to being firing large pieces of foam insulation at RCC panels and carrier panels at various angles of incidence to determine what sort of damage might have occurred during launch. The foam will be fired from a nitrogen gas canon at impact velocities of around 500 mph.
An RCC panel and upper and lower carrier panels taken from the prototype shuttle Enterprise will be heavily instrumented to determine impact stresses. An RCC panel taken from the shuttle Discovery, which has flown 30 times and closely matches the original-equipment panels that were on Columbia for its 28th flight, also will be subjected to foam impact for a more realistic assessment of what might have happened to Columbia. In addition, foam will be fired at so-called acreage tile, that is, normal heat-shield tiles located in the presumed foam debris footprint just behind the lower carrier panels.
In the meantime, NASA and CAIB investigators are continuing detailed chemical and metallurgical analysis of recovered debris to decipher complex damage patterns in hopes of pinning down the breach location and plume propagation path.
Mark Tanner, an expert in failure and forensic analysis with Mechanical and Materials Engineering, said "what we're trying to do is get an idea from the flow patterns, the splatter patterns and the deposits, where was the breach, where was the origin this whole thing started from. Or origins."
Complicating the picture is the ever present problem of determining when the observed damage occurred.
"A key question when we're looking at these pieces is with the damage we see, was it caused by something that happened on ascent, on descent, breakup or ground impact," Kovacs asked. "A lot of these pieces, you look at them and there's pine needles embedded in them. So clearly that did not happen in space and we're taking great care to understand the relationships of those issues."
All in all, he said, "there's a lot of jigsaw puzzling going on out there. It is like putting together a multi-thousand piece 3D jigsaw puzzle on a 2D surface."
So far, some 54,000 pounds of shuttle wreckage have been recovered, or about 24 percent of Columbia's 223,000-pound dry weight. That total represents 45,762 different parts or pieces of debris, of which just 1,406 have been laid out on a grid mapping the shuttle's lower surface. Dozens of RCC fragments have been found, but most have not yet been precisely identified as to their original location. Almost nothing from the RCC panel 6 location has been recovered, but sections of adjacent panels, along with RCC support hardware, are under analysis.
Engineers believe between 35 percent and 50 percent of the shuttle actually made it to the ground. The rest presumably burned up in the atmosphere following breakup, including virtually all of the aluminum skin structure of the wings.
"A lot of the parts have come through an aluminum molten rain cloud if you will, where they have aluminum splatter over much of the debris," NASA test director Steve Altemus said of the wreckage recovered to date. "We see that molten aluminum on almost everything we have back. It may also speak to why we don't have upper wing surface on the left wing in that that's very thin aluminum. So yes, we expect a great deal of the aluminum not to have made it to the ground."
Asked if anything unusual leaps out under casual inspection, Altemus said "what did strike me as odd, first of all, is the size of the pieces, how small they actually are, and also there's very little left wing lower surface structure and very little left wing upper surface structure. When you walk the grid, hat's what you notice, what is not present as opposed to what is there."
In any case, with spring blooming fast approaching, NASA expects to conclude its massive ground search in the next four to six weeks.
"As the spring comes on, the undergrowth begins to leaf out and the canopy begins to cover," said Michael Rudolphi, deputy director of NASA's Stennis Space Center. "Obviously, the first area you'll lose search capability will be from the helicopter. And then on the ground, as the brambles and the briars begin to leaf out, it's going to damage our ability to see and to identify any material on the ground.
"The forest service thinks we've got another four to six weeks before that becomes real serious," he said. "But ... it is already starting to green up. And It will impair our ability to find as much as we would like to find. There is a time element to do the thoroughness we would like to do. Obviously, we can keep walking around in the woods after it's greened up and we can keep looking, we just won't be as successful."
Shuttle debris fell in a 4- to 5-mile-wide footprint stretching some 250 miles across central Texas and western Louisiana. The debris field impacts some 169 counties in Texas and 39 in Louisiana. Of that total, 143 Texas counties have been searched, 10 counties are in the process of being searched and 26 remain to be searched. Thirty one Louisiana counties have been cleared with eight left to go.
While some 1,800 potential targets have been found on lake bottoms in the debris field using sonar, no major pieces of wreckage have yet been recovered by divers. And no debris has been found west of Texas.
Two flatbed truckloads of debris, each one carrying about 4,000 pounds of wreckage, arrive at the Kennedy Space Center each week. It is then examined, identified and bar coded and analyzed. A two-dimensional reconstruction of the shuttle's lower surface is being laid out on a grid in a 40,000-square-foot hangar near the shuttle landing facility.
Analysts are in the process of developing a computerized three-dimensional virtual reconstruction that will show recovered debris modeled on an imaginary orbiter much like aircraft wreckage is sometimes reassembled to aid visualization and to map out the actual locations of various pieces of debris.
"There are a couple of hundred small pieces of RCC panels," Tanner said. "This would be like putting together a solid gray puzzle. What complicates this is in some cases the fractures that would mate normally really well have been eroded away. So it is going to be a time consuming process of putting this together."
Just how long it might take is anyone's guess at this point.
"We're doing our very best. But this is the first time in human history anyone's had to analyze a hypersonic space re-entry disintegration of a craft," Kovacs said. "And so there's no one to ask how long will it take. And there's nothing out there on the floor I look at and go, well, it's going to be another month and we're out of here."
Even so, he said, "I'm very optimistic. I think we're going to be able to figure it out. We feel pretty confident."
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