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COVART
HOST SYSTEMS: SUN, SGI, PC
PROGRAM LANGUAGE: FORTRAN 77
The Computation of Vulnerable
Area Tool (COVART)
model predicts
the ballistic vulnerability of vehicles (fixed-wing,
rotary-wing, and ground targets), given ballistic penetrator
impact. Each penetrator is evaluated along each shotline
(line-of-sight path through the target). Whenever a critical
component is struck by the penetrator, the probability that
the component is defeated is computed using user defined
conditional probability-of-component dysfunction given a hit (Pcd/h)
data. COVART evaluates the vulnerable areas of components,
sets of components, systems, and the total vehicle. In its
simplest form, vulnerable area is the product of the presented
area of the component and the Pcd/h data. The total target
vulnerable area is determined from the combined component
vulnerable areas based upon various target damage definitions.
COVART is capable of modeling
several penetrators: a single missile fragment, a set of
missile fragments, a single Man Portable Air Defense (MANPAD)
missile, a single Armor Piercing Incendiary (API) projectile,
and a single High Explosive Incendiary (HEI) projectile. The
penetrator data used within COVART for vulnerability analyses
is documented within the Gun Pedigree report and the Missile
Pedigree report.
COVART is capable of modeling
the damage mechanisms induced by threat penetrators. Damage is
modeled using several methods. Analysts’ selection of the
damage mechanism modeling method is dependent upon the
penetrator type and failure modes of the equipment being
modeled. Physical damage criteria, such as hole size or damage
distance, are preferred because they can be directly related
to tests. Distance criteria are used to model blast and
hydrodynamic ram induced damage. Hole size criteria is used to
model functional failures due to liquid leaking from a
container. Air-gap distance criteria are used to model
sustained fires from threat induced leaks of flammable
materials. Other equipment damage is modeled using penetrator
impact mass and velocity relationships. A given component may
be vulnerable to several damage effects. The COVART model uses
failure analysis trees (fault trees) to assess the cascading
effects of damage. The fault trees use data obtained from
ground simulators (flight controls simulators, hydraulic
system simulators, avionics coolant simulators, fuel system
simulators, electrical power simulators) to enhance the
robustness and quality of failure predictions.
The COVART configuration
control is defined in the configuration control plan.
Modifications / improvements to the COVART code are made
through the model manager. Configuration control is obtained
by periodic releases on CD-ROM. The model manager has
authority to implement three-digit version control numbers.
While two-digit version control numbers require configuration
control board approval. Users are encouraged to inform SURVIAC
or the model manager when they find code errors. Users need to
document errors using the Software Change Request (SCR) form.
Additionally, users are requested to document projects usage.
This documentation provides the model manager with data to
justify requests for headquarters funding.
The COVART User’s Manual,
Analyst’s Manual, Programmer’s Manual are comprehensive
documents that outlines model usage. The COVART documentation
is available with the model.
Detail and robust
verification and validation (V&V) is difficult to complete.
COVART routines are based upon a combination of empirical
equations, test data, and expert rules. COVART has been
spot-checked over many years and many different applications.
Therefore, the Model Manager has a reasonable confidence in
the code. Currently the documentation of these V&V activities
is incomplete. The COVART report contains a small set of test
cases. These test cases were designed to highlight specific
COVART features. These test cases were small in size to
simplify testing. Therefore, test cases did not demonstrate
code functions using a full-up target description database.
This type of verification is very difficult and time
consuming.
The Joint Aircraft
Survivability Program Office is funding the development of
selected test cases. These test cases will be compared against
COVART and Advanced Joint Effectiveness Model (AJEM).
COVART
requires data characterizing the threat; velocity, material
etc.
The
model also needs specific data on the materials and
thicknesses of aircraft components. Required inputs for the
critical components, for the kill level being analyzed,
include Pcd/h data and fault tree data for redundant
components. COVART accepts line-of-sight data from FASTGEN and
BRL-CAD computer programs. See the FASTGEN section for further
information on the relationship between the FASTGEN and COVART
Models.
The COVART
model determines the vehicle vulnerable area as a function of
the kill level. Numerous kill levels could be modeled. The
following sets of kill levels are related to operational
capabilities: KK kill level (immediate), K kill (less than 30
seconds), pilot has time to eject, A kill (less than 5
minutes), B kill (less than 30 minutes) and mission kill. A
listing and the location of vulnerable components can be
displayed.
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