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COMMERCE BUSINESS DAILY ISSUE OF OCTOBER 7,1998 PSA#2196Naval Air Warfare Center Aircraft Division, Contracts Department,
Building 129-2, Highway 547, Lakehurst, NJ 08733-5083 17 -- HLU-196D/E BOMB HOIST SOL N68335-99-R-0005 DUE 120498 POC L.
Stibich, 732-323-4771; Contracting Officer is J. Murtagh. The Naval Air
Warfare Center Aircraft Division Lakehurst intends to procure the
HLU-196D/E Bomb Hoist, which is used to load air launched ordnance on
various Navy and Marine Corps aircraft. The required basic quantity is
for three each pre-production bomb hoists, training, and various
technical data. There will be three option periods of 199 each units
during which a total of 597 each production units and various technical
data may be required. The three each pre-production units should be
ready for contractor testing within 540 days after contract award. The
first shipment of pre-production units for government testing should
be within 720 days after contract award. The first shipment of
production units should begin 180 days after release for production
(provided the option for production units has been exercised). The
electrically powered bomb hoist shall be capable of lifting air
launched stores to the wing stations of all Navy aircraft utilizing the
existing Single Hoist Ordnance Loading system. The hoist will be
deployed and operated aboard ship and land and must meet the following
objectives: Mission time -- 144 lifts/day, approximately 12 hours in
a ten day mission; Maximum load -- 1,500 lbs. Vertical; Lift rate -- 15
ft/min; Maximum lift height -- 12 ft; Compatible with -- FA-18, EA-6B,
F-14, P-3, and S-3 aircraft and all existing SHOLS equipment; Maximum
weight -- 105 lbs; Emergency manual override for lowering and lifting;
Fail safe free fall prevention; Ability to support load indefinitely;
Overload protection (2,200 lbs. maximum load); Self-contained;
Reliability -- MTBF-400 hours (200 hours minimum), MTTR 1.5 hours
maximum, and Maximum repair time 3.7 hours. The final design will be
subject to the following testing requirements: Performance;
Environmental (MIL-STD-810) -- Sand and dust, Rain, Temperature-140F
storage, 120F operation, -40F storage, -20F operation; Vibration; EMI;
Shock; and Tech Evaluation (suitability and supportability). NAWCADLKE
has developed a proof of principle (POP) hoist upon which the
performance specification will be based. The POP unit is powered by a
NiCad battery pack, a brushless DC motor with electrically released
brake. The motor transmits power through a 1:1 belt drive to 180:1 lobe
and cam gearbox containing a "NoBak" one way torque device. This in
turn drives the winch components of the existing HLU-196 B/E hoist.
Further development of this design is required in the following areas:
higher efficiency gearbox; slide in battery pack; battery charging
system; AC adapter; improved one way torque device; increased battery
life and capacity; design of operator's controls; a minimum weight
reduction of 20 lbs.; and a reduction in overall size. POP will be made
available for a demonstration if requested. Delivery shall be FOB
Origin. Small Business Set-Aside. Posted 10/05/98 (W-SN258583). (0278) Loren Data Corp. http://www.ld.com (SYN# 0141 19981007\17-0002.SOL)
17 - Aircraft Launching, Landing and Ground Handling Equipment Index Page
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