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Milstar
Artist's impression of a Milstar Block I spacecraft
ManufacturerLockheed Martin (prime, formerly Lockheed Missiles and Space)
Northrop Grumman (formerly TRW)
Boeing (formerly Hughes)
Country of originUnited States
OperatorU.S. Space Force
ApplicationsMilitary communications
Specifications
BusMilstar Block I
Milstar Block II
Launch mass4,500 kilograms (9,900 lb)
RegimeGeosynchronous
Design life10 years
Production
StatusOut of production
Active
Built6
Launched6
Operational5[citation needed]
Lost1
Maiden launchUSA-99, 1994-02-07
Last launchUSA-169, 2003-04-08

Milstar (Military Strategic and Tactical Relay)[1] is a constellation of military communications satellites in geosynchronous orbit, which are operated by the United States Space Force, and provide secure and jam-resistant worldwide communications to meet the requirements of the Armed Forces of the United States. Six spacecraft were launched between 1994 and 2003, of which only five were operational after launch; the third launch failed, both damaging the satellite and leaving it in an unusable orbit.

History

[edit]

Milstar Block I spacecraft, or Milstar Developmental Flight Satellite (DFS)-1 and -2, were designed with a Low Data Rate (LDR) payload in the +X wing of the satellite that broadcast in the Super High Frequency (SHF) and Extremely High Frequency (EHF) ranges, and also a classified communication payload in the -X wing. The DFS-1 satellite was launched on 7 February 1994 aboard the first Titan IV(401)A rocket, but with the classified -X wing payload deactivated. It was followed by the DFS-2 spacecraft on 7 November 1995. DFS-2 was similar to DFS-1, but the classified payload was replaced by ballast in the form of a precision machined aluminum block to maintain the weight and balance characteristics of the satellite. Both Block I satellites (USA-99 and USA-115) are still operational as of March 2025, over 25 years since they were launched.

The four later satellites were Block II spacecraft, which featured an additional medium data-rate payload. The first Block II satellite (DFS-3m, a hybrid mix of largely Block I support systems and LDR payload and a MDR (Medium Data Rate) Block II payload) was launched on 30 April 1999, using a Titan IV(401)B rocket. Due to a database error affecting the attitude control system of the Centaur upper stage of its carrier rocket, it was placed into a lower orbit than had been planned, and damaged by deployment at excessive rates. It could not be raised into its operational orbit due to fuel limitations. Its orbit was raised as much as possible to increase the expected lifetime and then it was permanently turned off after 10 days.[2][3] It was the third consecutive, and last, failure of a Titan IV rocket. The remaining three satellites (DFS-4, -5, and -6) were launched on 27 February 2001, 15 January 2002, and 8 April 2003.

The Milstar system consists of three segments; the space segment which consists of the six satellites, ground terminals and users, and stations to command and control the satellites. The Military Satellite Communications Systems Wing (MCSW) division of the Space and Missile Systems Center, located at Los Angeles AFB was responsible for development and acquisition of the Milstar space and mission control segments. The Electronic Systems Center at Hanscom AFB is responsible for the US Air Force portion of the terminal segment development and acquisition. The 4th Space Operations Squadron at Schriever SFB and the 148th Space Operations Squadron at Vandenberg SFB are responsible for providing real-time satellite control and communications payload management.

In August 2010 control of the Milstar system was transferred to the Advanced Extremely High Frequency program, in preparation for the launch of the first AEHF satellite, USA-214. Advanced Extremely High Frequency satellites are intended to replace Milstar.[citation needed]

Characteristics

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Milstar satellites provide secure, jam resistant, worldwide communications to meet the requirements of the United States military. They were built by Lockheed Martin Missiles and Space Corporation, at a cost of US$800 million each. Each satellite has a design life of 10 years. Six were built, of which five reached their operational geosynchronous orbits, and remain in service. Launches were made using Titan IV rockets with Centaur upper stages, and all six occurred from Space Launch Complex 40 at the Cape Canaveral Air Force Station. The satellites are designed to provide communications which are hard to detect and intercept, and to be survivable in the event of nuclear warfare.

The spacecraft have a mass of 4,500 kilograms (9,900 lb), and are equipped with solar panels which generate eight kilowatts of electric power to power its transponders. Both Block I and Block II satellites provide low data-rate communications at bandwidths between 75 bit/s and 2,400 bit/s, whilst the Block II spacecraft can also provide medium data-rate communications between 4.8 kbit/s and 1.544 Mbit/s. The satellites' uplinks operate in the Q band, while their downlinks operate within the K band. The uplink corresponds to the extremely high frequency band while downlink corresponds to the super high frequency radio band.[citation needed]

Spacecraft

[edit]
"USA-99" redirects here. For the World Cup, see 1999 FIFA Women's World Cup.
USA ID Name Block Launch date/time (UTC) COSPAR ID Rocket Remarks
USA-99 DFS-1 Block I 1994-02-07, 21:47:01 1994-009A Titan IV(401)A
USA-115 DFS-2 Block I 1995-11-06, 05:15:01 1995-060A Titan IV(401)A
USA-143 DFS-3M Block I/II hybrid 1999-04-30, 16:30:00 1999-023A Titan IV(401)B Launch failure
USA-157 DFS-4 Block II 2001-02-27, 21:20 2001-009A Titan IV(401)B
USA-164 DFS-5 Block II 2002-01-16, 00:30:00 2002-001A Titan IV(401)B
USA-169 DFS-6 Block II 2003-04-08, 13:43:00 2003-012A Titan IV(401)B

See also

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References

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[edit]
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Milstar

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from Grokipedia
Milstar, officially the Military Strategic and Tactical Relay satellite system, is a constellation of five geosynchronous communications satellites operated by the United States Space Force to provide highly secure, jam-resistant, and nuclear-survivable global voice, data, and imagery transmission for U.S. military forces.[1][2][3] The system features cross-linked satellites operating in extremely high frequency (EHF) bands, enabling robust command and control even under adversarial conditions such as electronic jamming or nuclear effects, with coverage spanning latitudes from 65 degrees north to south for near-continuous 24/7 service to joint forces.[4][5][6] Developed as a joint-service Department of Defense program in the 1980s and launched between 1994 and 2003 by contractors including Lockheed Martin, Milstar marked a pioneering advancement in protected satellite communications, with its first two satellites equipped for low-data-rate payloads and the subsequent three adding medium-data-rate capabilities for enhanced throughput.[3][7] While highly reliable and integral to strategic operations for over two decades, the constellation has been progressively augmented and succeeded by the Advanced Extremely High Frequency (AEHF) system, which offers greater capacity—up to five times that of the full Milstar fleet in a single satellite—reflecting evolving demands for higher-bandwidth protected links in modern warfare.[3][8][5]

Development and History

Origins and Strategic Rationale

The Milstar program originated from assessments in the late 1970s identifying deficiencies in the U.S. Air Force Satellite Communications System, prompting debates over successors such as the single-purpose Strategic Satellite System (STRATSAT). Congress rejected STRATSAT proposals between 1979 and 1981, leading to a Department of Defense review in 1981 that refined requirements into the Milstar concept, emphasizing integrated strategic and tactical relay capabilities across services.[9] The Air Force formally initiated the program in November 1981, forming a joint program office in January 1982 at the Air Force Space Division to incorporate technologies from entities like the Naval Ocean Systems Center and Lincoln Laboratory, ensuring interoperability for Army, Navy, and Air Force users.[9] Strategically, Milstar was positioned within President Reagan's fall 1981 strategic modernization initiative, which prioritized resilient command and control communications amid Cold War nuclear threats. The system aimed to deliver jam-resistant, nuclear-survivable satellite links using geostationary orbits, enabling secure wartime exchanges for the President, unified commanders, and high-priority military forces where terrestrial networks might fail.[9] This focus addressed vulnerabilities to Soviet anti-satellite weapons, electronic warfare, and electromagnetic pulses, providing low-probability-of-intercept signals at extremely high frequencies (EHF) for global coverage without reliance on vulnerable ground relays. In 1983, President Reagan elevated Milstar to the highest national priority status, allocating initial funding of $16 million in fiscal year 1982 for advanced space communications development, reflecting its role in bolstering deterrence through assured continuity of operations in contested environments.[10] The program's joint-service architecture further rationalized resource allocation, merging strategic nuclear command needs with emerging tactical demands to avoid service-specific silos, though early scoping adjustments in 1982-1983 balanced ambitious survivability goals against budget constraints.[9]

Program Implementation and Launches

The Milstar program implementation proceeded in phases, beginning with two Block I satellites equipped for low-data-rate (75-2400 bps) secure voice and data communications, followed by three Block II satellites incorporating medium-data-rate (up to 274 kbps) crosslinks and enhanced payload processing. Lockheed Martin Space Systems served as the prime contractor for the satellite buses, integrating payloads developed by Northrop Grumman (formerly TRW), with launches executed via Titan IVB/Centaur rockets from Cape Canaveral Air Force Station under U.S. Air Force oversight.[2][11][12] The first satellite (USA-108) launched successfully on February 7, 1994, achieving geosynchronous orbit after separation from the Titan IV upper stage.[13][5] The second Block I satellite (USA-112) followed on November 7, 1995, completing the initial constellation segment; both underwent on-orbit testing, with initial operational capability declared in July 1997 after validation of nuclear-hardened, jam-resistant links.[13][14][15] Block II implementation addressed post-Cold War requirements for higher throughput, with the third satellite (USA-150) launched on February 27, 2001, following multiple delays from payload integration and launch vehicle availability issues originally targeted for 1999.[13][16] The fourth (USA-165) lifted off January 15, 2002, and the fifth (USA-169) on April 8, 2003, both confirming medium-data-rate functionality during post-launch checkouts.[13][17] A sixth Block II satellite was procured but never launched, as program priorities shifted toward the Advanced Extremely High Frequency successor system.[12][4]
SatelliteBlockLaunch DateLaunch VehicleOrbit Outcome
USA-108IFeb. 7, 1994Titan IVB/CentaurSuccessful GEO insertion[13]
USA-112INov. 7, 1995Titan IVB/CentaurSuccessful GEO insertion[13]
USA-150IIFeb. 27, 2001Titan IVB/CentaurSuccessful GEO insertion[13]
USA-165IIJan. 15, 2002Titan IVB/CentaurSuccessful GEO insertion[13]
USA-169IIApr. 8, 2003Titan IVB/CentaurSuccessful GEO insertion[13][17]

Technical Specifications

Satellite Bus and Payload Design

The Milstar satellite bus, developed by Lockheed Martin as the prime contractor, features a unique three-box configuration that folds compactly for launch aboard Titan IV rockets and deploys in geostationary orbit.[18] This design supports a launch mass of approximately 4500 kg, with a designed operational life of 10 years, powered by two deployable solar arrays and batteries for energy storage.[18] Propulsion is provided by two R-4D-12 engines for orbit maintenance and station-keeping.[18] The bus integrates payloads from subcontractors, including Northrop Grumman for low data rate (LDR) components, enabling onboard processing to enhance survivability by minimizing reliance on ground stations.[19] Block I satellites, designated as developmental flight satellites (DFS-1 and DFS-2), incorporate an LDR payload capable of handling nearly 200 user channels for secure teletype and voice communications at data rates from 75 to 2400 bits per second.[18] The payload receives uplink signals via nine extremely high frequency (EHF) antenna beams at 44 GHz, demodulates them onboard using custom large-scale integrated circuits, and routes them to super high frequency (SHF) downlinks at 20 GHz or ultrahigh frequency (UHF) at 250 MHz.[6] [18] A V-band crosslink payload at 60 GHz facilitates inter-satellite communications, supporting global connectivity without terrestrial relays.[18] Block II satellites augment the LDR payload with a medium data rate (MDR) capability, enabling transmission rates up to 1.544 Mbps for real-time voice, video, and data over 32 EHF channels.[6] [20] The MDR payload includes eight independently steerable EHF antennas: two nulling antennas for jamming resistance and six distributed user coverage antennas (DUCAs) forming narrow spot beams for directed, secure links.[6] Onboard digital signal processing, utilizing 14 application-specific integrated circuits (ASICs) and 397 LSI circuits in CMOS technology, handles demodulation, user authentication, dynamic resource allocation, and bandwidth-on-demand routing.[6] The V-band crosslinks extend MDR functionality across the constellation, maintaining compatibility with the bus's autonomous operations hardened against nuclear effects and electronic warfare.[20]

Communication Architecture and Frequencies

The Milstar system's communication architecture centers on a constellation of geosynchronous satellites equipped with phased-array antennas and onboard processing to enable secure, low-probability-of-intercept voice and data transmission for military users.[6] It incorporates inter-satellite crosslinks operating in the 60 GHz V-band, allowing direct connectivity between satellites to form a global network without reliance on vulnerable ground relays, thereby enhancing survivability in contested environments.[6][18] The architecture supports both low data rate (LDR) payloads for highly secure, jam-resistant communications at rates up to 2,400 bps and medium data rate (MDR) payloads on Block II satellites for higher throughput up to approximately 1 Mbps per channel.[21] Milstar utilizes extremely high frequency (EHF) bands for its primary anti-jam capabilities, with uplinks at 44 GHz and downlinks at 20 GHz to minimize susceptibility to interference and detection.[21][20] Compatibility with legacy systems is provided through ultrahigh frequency (UHF) uplinks at around 300 MHz and super high frequency (SHF) downlinks, including crossbanded services such as EHF uplink to UHF downlink.[18][22] These frequency allocations, combined with frequency-hopping and nulling techniques via the phased arrays, ensure robust performance against electronic warfare threats.[2]
Frequency BandRangeRole
EHF Uplink44 GHzPrimary secure uplink for LDR/MDR payloads
EHF Downlink20 GHzPrimary secure downlink
Crosslink60 GHzInter-satellite connectivity
UHF~300 MHzLegacy compatibility uplink/downlink

Operational Capabilities

Global Coverage and Network Features

The Milstar constellation comprises five operational satellites in geosynchronous orbit at approximately 22,000 miles altitude, enabling continuous 24-hour coverage for secure communications between 65 degrees north and 65 degrees south latitudes.[1][4] This latitudinal range supports global operations for U.S. military forces across most populated regions, with the system's design prioritizing uninterrupted service for joint-service users including ground, airborne, maritime, and strategic platforms.[23][24] Satellite-to-satellite crosslinks form a core network feature, allowing direct inter-satellite data exchange and routing without reliance on vulnerable ground stations, thereby extending connectivity to achieve full global coverage even with partial constellation availability.[1] These crosslinks, operational since the deployment of Block II satellites, enable the constellation to function as an autonomous "switchboard in space," dynamically managing traffic for real-time voice, data, and teletype services across tactical and strategic command levels.[6][25] The network supports multi-service interoperability, with Block I satellites providing low data rate (LDR) communications up to 2.4 kbps across 192 channels in the extremely high frequency (EHF) band, while Block II introduces medium data rate (MDR) capabilities up to 274 kbps for enhanced throughput.[1][2] Onboard digital processing and signal routing facilitate secure, point-to-point links using narrow, highly directional beams, minimizing interception risks and optimizing bandwidth allocation for prioritized military traffic worldwide.[6][20] This architecture ensures resilient, end-to-end connectivity for command and control, even in contested environments, with the full constellation achieving operational maturity by 2003 following the launch of the final satellite on April 23, 2003.[26]

Survivability and Anti-Jam Measures

The Milstar constellation incorporates multiple hardening measures to enhance survivability against nuclear effects and physical threats. The first three Block I satellites (launched between 1994 and 1995) feature radiation hardening to withstand high-altitude nuclear bursts, including resistance to transient radiation upset and electromagnetic pulse, though these costly nuclear survivability elements were omitted from the four Block II satellites to reduce expenses. [15] [16] Crosslinks between satellites enable autonomous network operation without reliance on vulnerable ground stations, allowing reconfiguration in response to threats or failures. [4] [20] The mission control segment includes both fixed and mobile elements for redundancy and dispersal, ensuring command continuity even under attack. [1] Anti-jam capabilities are primarily achieved through the use of Extremely High Frequency (EHF) bands (20-40 GHz), which provide inherent low probability of intercept/detection (LPI/LPD) due to narrow beamwidths and atmospheric attenuation that limits ground-based jamming effectiveness. [27] Onboard processing in the payloads, including adaptive nulling antennas and signal processing, actively suppresses interference by directing nulls toward jamming sources while maintaining links to legitimate users; tests in 1996 verified these antennas' performance against simulated threats. [28] [22] Low Data Rate (LDR) payloads on all satellites support 2,400 bps secure voice and data with jam resistance via frequency hopping and error correction, while Medium Data Rate (MDR) payloads on Block II satellites extend this to higher capacities (up to 1.544 Mbps in spot beams) with real-time processing for tactical environments. [20] [6] These features collectively ensure operation through nuclear or electronic warfare scenarios, prioritizing minimal essential command and control over volume. [29]

Controversies and Challenges

Cost Overruns and Congressional Scrutiny

The Milstar program experienced substantial cost growth throughout its development, with Department of Defense investments exceeding $5 billion from fiscal year 1981 to 1991 alone, prompting congressional demands for restructuring to achieve 25 percent savings in projected 20-year life-cycle costs.[30] By the mid-1990s, cumulative program expenditures approached $8 billion over 12 years, with each satellite costing approximately $1.3 billion, including $1 billion for the spacecraft and $285 million for launch, amid annual cost overruns estimated by critics at 35 percent.[10] These escalations stemmed from technical complexities in achieving jam-resistant, low-probability-of-intercept communications, as well as delays that pushed the timeline back by about five years, contributing to billions in excess spending beyond initial baselines.[10] Congressional scrutiny intensified in the early 1990s amid post-Cold War budget pressures, with the House Defense Appropriations Subcommittee slashing the fiscal year 1990 Milstar request by $632 million due to concerns over poor requirements definition, technical risks, and schedule slippages.[10] In July 1990, the Senate Appropriations Committee voted to eliminate the program's $1 billion funding for global nuclear-war communications capabilities, reflecting doubts about its necessity and affordability in a reduced-threat environment.[31] The National Defense Authorization Act for fiscal year 1991 directed either termination or major restructuring, leading to program modifications that reduced satellite numbers and emphasized cost-saving alternatives, though full cancellation was averted.[10] General Accounting Office reports amplified these concerns, highlighting in June 1992 that unresolved satellite issues—such as the cost-effectiveness of medium data rate payloads and unaddressed Army requirements for capacity and jamming resistance—necessitated a comprehensive cost-benefit analysis before approving further investments.[30] Terminal development costs also rose sharply, with Air Force command post units increasing from $5.2 million to $7.9 million each, alongside reliability shortfalls in Navy terminals (mean time between failures below 300 hours) and high risks in low-cost terminal designs lacking adequate testing.[30] By the late 1990s, disclosures of total life-cycle costs ranging from $35 billion to $40 billion, including over $1 billion annually in operations post-constellation, prompted additional congressional mandates for studies and efficiencies, though the program's strategic value in survivable communications ultimately sustained it through scaled-back procurement of five satellites.[15][10]

Technical and Schedule Difficulties

The Milstar program's development was marred by persistent technical challenges, particularly in terminal subsystems and payload performance. Navy shipboard and submarine terminals exhibited reliability shortfalls, achieving mean times between failures below 300 hours during operational tests in 1988 and 1990, which delayed full-rate production decisions pending additional reliability growth testing in 1992.[32] The Air Force's Low Cost Terminal encountered moderate to high risks in developing aircraft-compatible antennas and radomes, stemming from novel designs without established compatibility precedents, with fabrication deferred to the engineering and manufacturing development phase.[30] Satellite payload concerns included unproven capacity to meet minimum throughput requirements of 30.7 million bits per second, assured connectivity via dedicated access channels, and nulling antenna effectiveness against jamming threats, necessitating further analysis before major investments.[30] Schedule delays compounded these issues, originating from the program's outset. The initial target for launching and operating the first satellite slipped from late 1987 to early 1988 to February 7, 1994, a postponement of over six years attributed to integration complexities and technological maturation needs.[15] Subsequent launches faced setbacks, including delays for the fourth satellite due to Titan IV vehicle anomalies and malfunctions in the spacecraft's thrust heaters.[15] Software development lags for critical ground and terminal components further impeded tactical mission integration, while deferred oversight milestones, such as the absence of formal exit criteria for low data rate terminal engineering phases until a 1992 Defense Acquisition Board review, exacerbated timeline risks.[33][32] Delivery delays in encryption equipment from the National Security Agency also hindered payload readiness and overall system synchronization.[34] These factors contributed to broader program restructuring, with terminal production quantities—such as Army SCOTT units reduced from 330 to as few as 85—reassessed amid doubts over demand and integration feasibility with aircraft platforms.[30] Despite mitigations like risk reduction contracts and consolidated contractor responsibilities, the cumulative effect prolonged initial operational capability beyond early projections, highlighting the inherent difficulties in pioneering extremely high frequency communications with nuclear survivability features.[32]

Legacy and Impact

Achievements in Secure Military Communications

The Milstar constellation achieved unprecedented levels of secure military communications by integrating onboard signal processing and routing, which minimized reliance on vulnerable terrestrial infrastructure and enhanced resistance to interception and disruption. This design enabled the system to function as a self-contained "switchboard in space," supporting voice, data, and teletype communications for strategic and tactical users across global operations.[2][35] By employing extremely high frequency (EHF) bands with frequency-hopping techniques, Milstar provided jam-resistant links capable of operating through nuclear effects and enemy denial efforts, marking a foundational advancement in protected satellite systems.[36] In operational contexts, Milstar demonstrated reliability during high-stakes conflicts, including Operation Iraqi Freedom, where it facilitated secure transmission of critical command and control information for U.S. forces amidst contested electromagnetic environments. The system's robustness allowed national leaders and field commanders to maintain connectivity through all conflict phases, from strategic planning to tactical execution, without interruption from adversarial jamming.[37] Sustained performance metrics underscored this capability, with the five-satellite constellation accumulating over 50 years of combined on-orbit operations by 2009, exceeding design life expectations while delivering consistent uptime.[12] Milstar's longevity further highlighted its engineering triumphs, reaching 25 years of service by 2019 and 30 years by 2024, during which it remained the U.S. Department of Defense's most advanced protected communications network. This endurance validated the program's focus on survivability, as the satellites continued to support no-fail missions despite evolving threats, influencing subsequent systems like AEHF.[5][38] The constellation's operational success affirmed its role in ensuring assured access to space-based communications, even under nuclear or electronic warfare conditions, thereby bolstering U.S. military superiority in information dominance.[11]

Transition to Advanced Systems

The Milstar constellation, comprising five satellites launched between 1994 and 2003, established a baseline for protected extremely high frequency (EHF) communications but faced limitations in data throughput and capacity amid growing demand for higher-bandwidth secure links in modern warfare.[1][12] To address these constraints, the U.S. Air Force initiated the Advanced Extremely High Frequency (AEHF) program in the late 1990s as Milstar's direct follow-on, aiming to deliver ten times the information throughput, expanded global coverage, and enhanced anti-jam resilience while maintaining backward compatibility with existing Milstar terminals.[39][40] A pivotal step in the transition occurred on August 3, 2010, when the Air Force and Lockheed Martin shifted day-to-day operations of the Milstar constellation to the AEHF Mission Control System (MCS), consolidating command and control under a unified ground segment capable of managing both legacy and new satellites.[3] This integration enabled seamless cross-linking; for instance, AEHF-1, launched in August 2010 and declared operational in 2011, began relaying traffic with Milstar satellites, demonstrating interoperability.[41] By 2012, AEHF-2 further expanded the network, and the three-satellite AEHF core achieved full operational capability on August 10, 2015, augmenting Milstar's role in high-priority strategic communications.[42] The AEHF program's completion of Milstar's command-and-control handover by December 2019 marked the effective phasing of legacy operations into the advanced framework, with AEHF-5 and AEHF-6 launches in 2019 and 2020 finalizing a six-satellite constellation that operated until the program's close in January 2021.[40][39] This evolution preserved Milstar's emphasis on survivability—such as nulling antennas and low-probability-of-intercept signals—while scaling capacity for tactical users, including compatibility with Secure Mobile Anti-Jam Reliable Tactical Terminal (SMART-T) systems that bridged Milstar and AEHF waveforms.[43] Subsequent U.S. Space Force efforts, including proliferated low-Earth orbit protected communications, build on this foundation but retain AEHF's core architecture for strategic resilience.[1]

References

  1. Milstar Satellite Communications System - Space Force
  2. Milstar Satellite Communications System
  3. U.S. Air Force/Lockheed Martin Team Transitions Operations of ...
  4. Milstar Satellite Communications System
  5. Milstar program reaches 25 year milestone - U.S. Strategic Command
  6. Milstar Payloads - Northrop Grumman
  7. U.S. Air Force/Lockheed Martin-led Team Celebrates Success of ...
  8. Lockheed Martin-Built AEHF-5 Protected Communications Satellite ...
  9. [PDF] Case Study of the MILSTAR Satellite Communications System
  10. [PDF] thesis - DTIC
  11. The Amazing MILSTAR Constellation—20 Years Of Service
  12. Five-Satellite Milstar Constellation Built by Lockheed Martin ...
  13. Milstar Satellite Communications System - Space Force
  14. Milstar Satellite Communications System Archives
  15. [PDF] MILSTAR Satellites - Archived 2/2006 - Forecast International
  16. Milstar
  17. New Milstar launches from Cape - AF.mil
  18. Milstar-1 1, 2 (Milstar 1, 2) - Gunter's Space Page
  19. Second Milstar Satellite Built by Lockheed Martin Achieves 10 Years ...
  20. Milstar-2 1, 2, 3, 4 (Milstar 3, 4, 5, 6) - Gunter's Space Page
  21. [PDF] EHF/SHF (Super High Frequency) SATCOM (Satellite ... - DTIC
  22. The Milstar system - AIAA ARC
  23. Milstar Satellite System - FY97 Activity - GlobalSecurity.org
  24. (U) Milstar I
  25. Lockheed Martin-Built Milstar Satellite Constellation Repositioned to ...
  26. U.S. Air Force Ready to Launch Last Lockheed Martin-Built Milstar ...
  27. (U) Milstar II
  28. TRW completes tests on Milstar anti-jam antenna | News | Flight Global
  29. MILITARY STRATEGIC AND TACTICAL RELAY (MILSTAR ...
  30. [PDF] Milstar Program Issues and Cost-Saving Opportunities - GAO
  31. SENATE COMMITTEE CUTS PENTAGON TROOPS, ARMS
  32. [PDF] Military Satellite Communications: Milstar Program Issues ... - DTIC
  33. [PDF] MILITARY SATELLITE COMMUNICATIONS - GovInfo
  34. Bandwidth Breakthrough | Air & Space Forces Magazine
  35. U.S. Air Force/Lockheed Martin-led Team Celebrates Success of ...
  36. Milstar - Army Technology
  37. Smithsonian Institution Honors Lockheed Martin-Built Milstar ...
  38. MILSTAR celebrates 30 years of secure communications - DVIDS
  39. End of an Era: The AEHF Program comes to a close
  40. [PDF] Advanced Extremely High Frequency Satellite (AEHF)
  41. Air Force begins testing newest AEHF satellite - AF.mil
  42. U.S. Air Force Declares Three-satellite AEHF Constellation ...
  43. Final production of protected satellite terminals postures ... - Army.mil
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