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National security requirements dictate a continuing, highly reliable means of
placing critical DoD satellites into required orbits. The Titan IV system can launch the
largest of these satellites into near-earth or geosynchronous orbits from either the east or
west coast launch facilities. Titan IV has several configurations: No Upper Stage (NUS),
Inertial Upper Stage (IUS), and Centaur; also the Titan IVB, with solid rocket motor upgrade
(SRMU) and new avionics and ground support to meet reliability and increased performance
requirements. The program is acquiring 41 Titan II and IV launch vehicles.

Key Program Factors:
Program provides continuing integration support to the
payload community, as well as continuing engineering support to maintain system characterization
and reliability
Since 1994, the Titan IV program has also included funding
for Titan II engineering costs, payload integration, and Government costs
Acquisition Service and
Category: Air Force, ACAT-1D
A new acquisition strategy transitions from the current
41-vehicle development/production and payload integration contracts to new contracts designed
to improve cost accountability, correct contract discrepancies, and define the total effort to
complete the program. This strategy combines Titan II and IV production, storage, launch pad
maintenance and deactivation, launch operations, anomaly resolution, development and hardware
requalification, payload integration and program studies to save costs by maximizing use of
resources and eliminating duplication.
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Major contractors:
Lockheed Martin Aerodynamics and Astronautics, Denver, CO (prime); Aerojet, Sacremento, CA, (liquid rocket engine [LRE]); McDonnell Douglas, Huntington Beach, CA (payload fairing); Alliant TechSystems, Magna, UT (SRMU); United Technologies, San Jose, CA (
SRM); Honeywell, Clearwater, FL (avionics).
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