|
COMMERCE BUSINESS DAILY ISSUE OF FEBRUARY 25,1997 PSA#1789United Defense LP, Armament Systems Division, 4800 E. River Rd.,
Minneapolis, MN 55421-1498 59 -- EQUIPMENT TO DETERMINE PROPELLANT TEMPERATURE POC Point of
Contact: John Hornseth, M387, (612) 572-6634, INTERNET:
john_hornseth@fmc.com WEB: United Defense LP,
http://www.fmc.com/crusader. E-MAIL: United Defense LP,
john_hornseth@fmc.com. United Defense, L.P., Armament Systems Division,
under Prime Contract DAAE30-95-C-0009 is gathering information on
potential suppliers of equipment to determine the temperature of MACS
(Modular Artillery Charge System) solid propellant used to fire the
155mm cannon on the Crusader SPH (Self Propelled Howitzer). The
propellant temperature is used to predict projectile muzzle velocity in
order to achieve down range accuracy. The MACS consists of two types of
combustible case charges (XM231 and XM232) that are loaded into the gun
tube in various quantities to achieve the desired muzzle velocity to
accurately deliver the projectile to the target. Loading, storage, and
other handling of the MACS is performed by automated handling
equipment on board the Crusader SPH. Both charge types are cylindrical
in shape with approximate dimensions of six inches in length and six
inches in diameter. Simply described, the construction consists of the
propellant encased in a cylindrically shaped outer combustible case
body. The case body formulation is mainly nitrocellulose and has a wall
thickness of 0.10 inch. Current gun systems measure propellant
temperature directly by manually penetrating the outer bag with a
temperature probe. This data is periodically updated to the fire
control system. In this method it is assumed that the propellant
temperature has stabilized and that a direct measurement of the
propellant on a periodic basis suffices in achieving the desired muzzle
velocity prediction. To achieve better muzzle velocity predictions for
Crusader, propellant temperature will need to be determined for every
MACS charge. Further, it cannot be assumed that the propellant
temperature has stabilized. Due to the low thermal conductivity of the
propellant, significant temperature gradients are expected from the
core to the outer case on the order of magnitude of tens of degrees
Celsius. Therefore, measuring the outer case temperature will not
necessarily determine the propellant temperature and directly measuring
the propellant temperature at one location will not characterize the
temperature gradient. The ideal measurement device will meet the
following operational requirements: 1. Provide an accurate
characterization of the effective propellant temperature accounting for
temperature gradients between the core and outer case body. (order of
magnitude of 1-2 degrees celsius) 2. Determine the temperature quickly
(order of magnitude of 1 second) 3. Determine the temperature in a
non-invasive and non-destructive manner. 4. Operate in the environment
of a military ground vehicle. 5. Operate fully automatically with no
soldier intervention. Potential qualified suppliers are requested to
submit a capability statement to John Hornseth, in writing, at M387,
INTERNET at john_ hornseth@fmc.com or by facsimile at 612-572-4991
within 21 calendar days of the publication of this announcement.
Capability statements can be in supplier format, and should include, at
a minimum: 1. A narrative discussion or report addressing the current
status and performance of the candidate equipment being proposed along
with supporting data. 2. A narrative discussion of the unique
technical capabilities and expertise of the organization. 3. A
narrative discussion supporting the organization's ability to meet the
development schedule of the candidate equipment (2 units plus spare
parts) to be delivered to United Defense no later than December 1998.
Respondents to this notice will not be notified either of the receipt
or the assessment of the information submitted. Neither the cost of
preparing capability statements nor the cost of preparing proposals
will be entertained as allowable direct charges to any resultant
subcontract. This solicitation does not obligate United Defense, L.P.
to enter in any purchase agreement with any organization supplying
information. (0052) Loren Data Corp. http://www.ld.com (SYN# 0384 19970225\59-0017.SOL)
59 - Electrical and Electronic Equipment Components Index Page
|
|