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COMMERCE BUSINESS DAILY ISSUE OF MAY 23,1997 PSA#1852HSC/YAK, 8107 13th St, Brooks AFB, TX 78235-5218 84 -- COMMERCIAL OFF-THE-SHELF (COTS) SECONDARY RESTRAINT DEVICE FOR
THE ADVANCED TECHNOLOGY ANTI-G SUIT DUE 060697 POC Ms. Susie Madrid,
Contract Specialist, HSC/YAK, (210) 536-6337 The Life Support Division
at the Human Systems Program Office, Brooks AFB, TX is contemplating
the acquisition of a Commercial-Off-The-Shelf (COTS) device to use as
a secondary restraint for a lower body pressure garment (anti-G suit)
for wear by aircrews of high performance aircraft. This announcement is
not a formal solicitation and is not a request for proposal. Any formal
solicitation will be announced separately. This synopsis is for
information and planning purposes only and is not to be construed as a
commitment by the Government. The intended operating environment for
the anti-G suit is in high performance aircraft such as the F-15, F-16,
and F-22. The anti-G suit pressurizes up to 12 psig under the effects
of high positive acceleration (G) in the Z axis to prevent vascular
pooling of blood in the lower body. The suit consists of a continuous
bladder contained inside layers of fabric. The primary restraints for
the pressurized bladder are full length zippers which run from the
upper thigh to ankle level on the inside of each leg. The purpose of
the secondary restraint is to contain the bladder in the event of
failure of the primary restraint, since unconstrained expansion of the
bladder could result in interference with aircraft flight controls
and/or other aircrew functions. The secondary restraint device would be
attached to the exterior fabric of the suit. The current design of the
suit uses plastic, squeeze-to-release buckles (like those used on
backpacks/luggage) as the secondary restraint device, with three
buckles on the inside of each leg (two on the thigh, one on the calf).
The buckles in the current design attach to the suit with cloth straps
underneath the primary restraint zipper. These buckles exhibit most of
the required attributes, but do not have sufficient tensile strength.
The required attributes of the secondary restraint device (not
necessarily a buckle) are as follows: small size (approximately 1" wide
by 2 and 1/2" long by 1/4" deep); lightweight (maximum of 180 grams
total for the suit); capable of withstanding at least 500 pounds of
tension for 15 seconds; will not inadvertently open; durable (will
withstand 6000 inflation cycles of the suit to 12 psig); must withstand
3000 connections/disconnections; shelf life of 10 years; must not
degrade compatibility with the cockpit or with other aircrew personal
equipment; must fit the full range of the male/female aircrew
population; must not inhibit aircrew movement in and out of the
cockpit; must not inhibit emergency egress from the aircraft; must be
ejection compatible (withstand a 600 knot windblast); comfortable for
long duration wear; quick/easy to don and doff without assistance; must
function without interfering with the pockets on each lower leg; must
be non-corrosive; must be capable of field level replacement in 30
minutes or less without requiring the use of special tools; must be
launderable; must be decontaminable; and must operate at temperatures
of -40 to +125 F after storage between -60 to +160 F at up to 100%
humidity.Technical discussions on secondary restraint systems submitted
for consideration should include technical specifications, operating
instructions, a drawing(s), and test documentation supporting the
performance of the item with regard to the desired attributes listed.
Information on past or current users of the item (customer list, points
of contact and phone numbers) should be presented, along with the
application(s) the item was used for. Price information to include
current catalog prices should be provided, and should be based on the
quantity of secondary restraint devices required to equip 50 suits for
testing, as well as production lots to equip 1,000 suits; 2,000 suits;
and 5,000 suits. The response time (delivery date) for sufficient
devices to equip the 50 test suits should be stated. Written responses
and hardware samples, if available, sufficient to equip one anti-G
suit are due not later than 3 June 1997. Telephone responses will not
be honored. There is no specific format for responses; however,
information submitted should be relevant to the contemplated
acquisition. Hardware samples submitted to the Government will not be
returned. Firms responding should indicate whether they are a small
disadvantaged business (SDB), 8(a), small business, or large business.
Responses should be addressed to Human Systems Center (HSC/YAK); Attn:
Mrs. Susan M. Madrid, 8107 13th Street, Brooks AFB, TX, 78235-5218.
(0141) Loren Data Corp. http://www.ld.com (SYN# 0387 19970523\84-0003.SOL)
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