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COMMERCE BUSINESS DAILY ISSUE OF JUNE 27,1995 PSA#1376Aeronautical Systems Center, Weapons, Air Base and Range Product
Support Organization, 102 West D Avenue, Suite 300, Eglin AFB FL
32542-6808 A -- DESIGN, DEVELOPMENT, AND DELIVERY OF TRANSLATED GPS RANGE SYSTEM
(TGRS) EQUIPMENT POC Mr. Lee Powell, Contract Specialist,
904/882-8601, Ext 317 Ms Tanya Lambert, Program Manager, 904/882-8601,
Ext 352. Design, development, and delivery of the Translated GPS Range
System (TGRS). This announcement is the precursor to the release of the
Draft Request for Proposal (DRFP) for the TGRS. The contractor shall
deliver equipment as indicated: Digital GPS Translators (DGTs) to
various Department of Defense (DOD) Users and Ranges, GPS Translator
Processors (GTPs) to various DOD Users and Ranges. Options to the
contract will provide DGTs, GTPs, predetect recorders, repair kits,
field engineering support, etc., to various DOD Users and Ranges. The
TGRS shall meet the following requirements: 1) shall be capable of
operation in ballistic or tactical missile host vehicles subjected to
100 g acceleration (goal is 150 g acceleration), 100 g/sec jerk (goal
is 150 g/sec jerk), and 30,000 ft/sec velocity, The TGRS shall be
composed of three major elements: the Participant Segment, the Relay
Segment, and the Range Segment. The Participant Segment shall be
mounted in a missile or other host vehicle under test. This segment
shall provide accurate reception, frequency translation, digitization,
and encryption of GPS Satellite Vehicle (SV) signals. This segment
must also provide for secure transmission of other host vehicle
telemetry signals (up to 16 Mbits/sec) in addition to and merged with
transdigitized GPS signals with a maximum data rate of up to 20
Mbits/sec. The combined data rates will not exceed 20 Mbits/sec. This
segment shall consist of the DGT and Power Booster Unit (PBU) whose
combined size shall not exceed 10 cubic inches. The Relay Segment shall
be mounted in an airborne relay platform. This segment shall provide an
over-the-horizon (OTH) link between the participant segment and the
range segment. This segment shall consist of a GTP which receives and
processes participant segment signals, provides real-time TSPI state
vectors for the host vehicles and transmits this data to the range
segment. The Range Segment shall be mounted at a fixed reference ground
site, or optionally in an airborne or shipborne reference vehicle. This
segment shall provide real-time TSPI for participant vehicles by
processing line-of-sight (LOS) translated GPS signals from participant
segment components and OTH relayed signals from the relay segment
components. This segment shall also provide enhanced post-flight
trajectory analysis for participant vehicles by processing LOS
translated GPS signals. This segment shall consist of the GTP, a
Mission Control Console (MCC),a Predetect Signal Recorder (PSR), and a
reference receiver antenna/preamplifier. The TGRS must satisfy the
following key technical requirements and characteristics: (a) shall
provide real-time and post-mission GPS dual band (L1/ L2) processing
and secure signal transmission from host vehicle to the GTP, (b) shall
be capable of supporting digital translators (goal is analog and
digital), (c) shall be capable of detecting and eliminating unhealthy
GPS satellites from the real time state vector solution, (d) shall be
capable of all-in-view GPS satellite tracking, (e) shall be capable of
real time processing of tracked vehicle state vector updates at a
selectable 1, 10 or 20 times per second, (f) under the maximum dynamics
listed above, shall provide real-time state vector solution accuracy
not to exceed 9.0 m horizontal position, 16.0 m vertical position, 2.0
m/sec horizontal velocity, and 3.3 m/sec vertical velocity, (g) under
more benign dynamics (10 g/sec jerk), shall provide real-time state
vector solution accuracy not to exceed 4.1 m horizontal position, 6.8
m vertical position, 0.15 m/sec horizontal velocity, 0.25 m/sec
vertical velocity, (h) under the maximum dynamics listed above, shall
provide sub-meter accuracy enhanced post-mission trajectory analysis,
(i) shall simultaneously acquire and establish track of multiple (4
required, 8 is goal) vehicles with the dynamic vehicle tracking
accuracies specified above within 3 seconds of launch without prior
knowledge of nominal or actual vehicle position and velocity, (j) shall
be capable of accepting and outputting baseband signals from the
tracked vehicle to and from a predetect recorder, (k) the GTP shall be
capable of accepting data concurrently from both right-hand and
left-hand circularly polarized S-band antenna feeds, aligning the pilot
carrier phases, selecting the better signal in real time, and recording
the two signals independently, (l) shall meet EMI/EMC requirements, (m)
the GTP shall be a maximum of 10 inches in height and be configured to
mount in no larger than a standard 19-inch rack, (n) the GTP shall be
equipped with a self-contained P-code GPS reference receiver, (o)
shall be designed as a turn-key system, (p) shall have the capability
of post mission processing of recorded mission data, (q) shall be .999
reliable, (r) the GTP shall be capable of receiving and processing
translated GPS S-band signals from 2200 to 2400 Mhz in 1 Mhz steps with
polarization diversity, (s) shall have selective
availability/anti-spoofing (SA/A-S) capability, (t) shall be capable of
supporting host vehicle L-band patch (switching) antenna
configurations, (u) shall be supportable under a two-level maintenance
program, (v) shall be capable of being remotely configured and
operated except for data retrieval to a removable storage medium, (w)
shall be capable of simultaneously tracking multiple host vehicles in
flight. A technical data package is not available. Interested sources
must demonstrate the following capabilities: (a) Delivery schedule is
of the essence. System must be qualified and delivered by October 1997
to support planned user testing in the 3rd quarter FY98, (b) Must have
developed and utilized Translator Processing Systems in the support of
Government tests which used GPS translators to track ballistic objects
in space, (c) Must have total system and product support capabilities
(e.g. reliability, manufacturing and producibility, human engineering,
logistics support analysis, training and technical manuals). (d) Must
have proven capability to conduct formal program, technical, and test
reviews (e.g. Preliminary Design Review, Critical Design Review,
Functional Configuration Audit, Test Planning Working Group). (e) Must
have a quality control and quality assurance system in place. (f) Must
have an in-place field service organization to provide up to three
years of product support for equipment delivered to Department of
Defense ranges. The contractor shall provide on-call field engineering
and technical support to the Government in order to operate and
maintain the TGRS equipment located at the applicable ranges. The
contractor shall supply all labor, services, supplies, support
equipment, and technical data. Firms requiring associated data are to
provide names of personnel requiring access and validate their
capability to receive Scientific and Technical Information (STINFO)
under 22 U.S.C. 2751 and U.S.C. 50 Appendix 2401. It is unlawful to
export items containing export controlled technical data. Potential
contractors will be required to obtain certification from the Defense
Logistics Services Center (DLSC), Battle Creek MI 49016-3412, telephone
1-800-352-3572 in accordance with DOD 5230.25 prior to being provided
access to unclassified data. Certification is accomplished using DD
Form 2345, Military Critical Technical Data Agreement. This requirement
for DD Form 2345 certification also applies to any subcontractors being
given access to reproduced data by another contractor. It is not the
intent of the Government to obtain proprietary information by means of
this synopsis. Any hardware or services which the Government may elect
to procure as a result of responses to this announcement will be
announced separately. All documents for TGRS will be available in
Microsoft Word 6.0 on the Eglin Bulletin Board for downloading by
potential bidders. The Eglin Bulletin Board telephone number is (904)
882-5310. Information and particulars to document your capabilities and
qualifications to satisfy the TGRS effort must be submitted to
ASC/VXGK, ATTN: Lee Powell, 904-882-8601 Ext 317. Closing data for
submission of particulars is 15 days after publication of this notice.
This synopsis is for information and planning purposes only and does
not constitute an IFB or RFP and is not to be construed as a commitment
by the Government. After statements of capability have been screened,
an RFP may be issued to those prospective sources who, in the sole
judgment of the procuring activity, have the potential to successfully
fulfill the stated requirements. (0174) Loren Data Corp. http://www.ld.com (SYN# 0006 19950626\A-0006.SOL)
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