1998 Army Science and Technology Master PlanA technology taxonomy has been developed to define the core technology capabilities in SMDC. Part of the commands missions and goals is tied directly to the development of advanced technology, as well as the support of the FOCs of the warfighter and the demonstration of "bundled" technology capabilities to defeat the projected threats discussed in subsection C. These technologies have been broken into eleven technology areas and subareas, which are discussed below.
a. Kinetic Energy Weapons Technology
HittoKill (HTK) Miniature Interceptor. The advanced submunitions (AS) threat has received significant attention recently in the defense community as a potentially effective countermeasure to those TMD systems currently in development, such as theater highaltitude area defense (THAAD) and Navy upper tier. The AS countermeasure appears to be easy to implement (BMDO SM2 experiment) and could be a validated threat by the year 2002. The submunitions could be either conventional, chemical, or biological. The HTK miniature interceptor is a multiplekill vehicle concept intended to counter this threat. It is based on advanced component technologies under development with BMDO funding, which are integrated into extremely small kill vehicles, thereby allowing many to be carried aboard a single interceptor. The HTK miniature interceptor concept would be designed to be compatible with the baseline TMD concept of operation using the same radar, booster, launcher, and BM/C3. However, the conventional killpayload would be replaced with a cluster of HTK miniature interceptors. A small fraction of the conventional interceptors in each fire unit would be replaced with interceptors filled with HTK miniature interceptor kill vehicles. The threat would be detected and tracked as in the conventional TMD scenarios. The TMD radar would determine the composition of the threat payload and, when needed, an interceptor with a cluster of HTK miniature interceptor projectiles would engage the submunitions in an exoatmospheric environment.
The current state of the technology and the technical innovations needed by the year 2002 and year 2015 is shown in Table D3.
Table D3. HittoKill Miniature Interceptor Technology Plan |
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System Element |
Current |
By 2002 |
By 2015 |
Innovations Needed |
| Propulsion & Steering | Impulsive diverters under development | >5 g | >40g | More maneuverable, responsive, and robust divert systems, miniature, low cost |
| Sensor | Single color passive sensor under development | Single color | Multicolor, multimode IR and RF with decoy resistance | Miniature, low cost, high resolution, low loss optics, shock resistant |
| Tracking | Star tracking experiment planned | Passive | Active/passive | High power laser diode, small and low cost |
| Terminal Guidance | Reticle based guidance under development | Reticle/proportional | FPA/advanced guidance (endoatmospheric) | Higher accuracy guidance algorithms and high data rate processors. |
| Integrated Kill Vehicle/Dispenser | No work to date | Transition to materiel developer | System fielded | Lightweight, spin rate control, dispenser induced pointing error |
Exoatmospheric Interceptor Technology (EIT). The EIT program will provide the only exoatmospheric interceptor technology testbed program for the development of fireandforget smart interceptors. This program will develop and integrate active and passive sensors, data fusion, lightweight avionics, highsensitivity low background focal plane arrays (FPAs) with highspeed hardened electronics, high acceleration and divert propulsion, and sophisticated onboard target track and discrimination capability. The testbed will serve to demonstrate the technology goals without development of new interceptor kill vehicles (KVs).
The EIT program includes coordinating and maintaining a complementary interceptor technology base for relevant components and subsystems, correlating its core technologies to ongoing ATDs, ACTDs, and acquisition programs. It also includes working through BMDO to coordinate the users and acquisition programs to identify, develop, and mature the technologies further.
Fireandforget smart interceptors directly support the Joint Vision 2010 of precision engagement, dominant maneuver, and fulldimensional protection. The testbed demonstrations of fireandforget exointerceptor target kills will be performed against responsive threat complexes. A series of endtoend, 6degreeoffreedom (DOF), hardwareintheloop (HWIL) simulations, ground, and flight tests will be performed with the integrated KVs. After successful demonstration of the integrated KV capability, the technology will be available for transitioning to the appropriate interceptor ACTD or acquisition programs. [POC: Robert Franklin, (205) 9555817, email: franklinb@smdc.army.mil]
These technologies will enhance existing interceptor capabilities and add new ones such as advanced inertial measurement units (IMUs) and batteries enabling longer flyout times. Advanced LADARs, FPAs, algorithms, and signal/data (S/D) processors will enable longer acquisition ranges and better discrimination. Advanced divert and attitude control system (DACS) will enable a much greater divert capability. The current technology capabilities, projected capabilities for 2009 and 2015, and innovations needed to achieve these capabilities are listed in Table D4.
Endoatmospheric Interceptor Technologies. The objective of AIT is to develop and demonstrate advanced lightweight technologies for hypersonic HTK intercept of threat missiles within the atmosphere and integrate these technologies into a small (130 cm3), lightweight (50 kg) KV. High velocity intercepts are essential to maintain sufficient battle space, lethality, and coverage/footprint performance. However, such conditions provide severe aerooptic, aerodynamic, aerothermal, and structural requirements. Jet interaction (JI) testing is providing insights into JI sensitivities to design
Table D4. Exoatmospheric Interceptor Technology Plan |
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Component |
Today |
2009 |
2015 |
Innovations Needed |
| IMU | 0.4kg IFOG with 4deg/hr bias stability, 10mg acceleration sensitivity | 0.5kg RFOG with 0.01 deg/hr bias stability, 100mG acceleration sensitivity | 0.4 kg RFOG with 0.001 deg/hr bias stability, 50mG acceleration sensitivity | Low loss optical connectors, low loss fibers, improved laser source, solidstate accelerometers, improved power management technology |
| LADAR | No interceptor LADAR available | 5kg, 300km range, solid state | 4kg, 500km range, solid state | Improved laser transmitters and receivers improved power management technology |
| FPA | 2562 MCT, nonrad hard on FPA readout electronics | 5122 , rad hard, multiwave band on FPA processing electronics | 10242 , rad hard, tunable waveband, high temperature on FPA processing electronics | Improved materials and processing techniques improved manufacturing techniques |
| Algorithms | Basic discrimination algorithms | Onboard active/passive discrimination, control system algorithms for maneuvering threats | Algorithms promoting autonomous launchandforget operation | Improved S/D processors |
| S/D Processors | Level2 hardened, 1012 IPS, 1012 OPS | Level2 hardened, 1014 IPS, 1014 OPS | Improved power management technology; improved chipset design and parallel processing technologies | |
| DACS | Army LEAP DACS subsystem | 200km divert capability, solid propellant, start/stop capability | 400km divert capability, solid propellant, start/stop capability | Higher Isp propellants, faster response, high temperature hot gas valves, high temperature nozzles |
| Boosters | Not available | Booster with composite motorcase, thrust vector control | Advanced composite integrated stage booster, thrust vector control | Higher Isp propellants, faster response, high temperature injector valves, higher strength fibers |
| Warheads | Conventional warhead, directionally fragmented | Explosive reactant, counter earlyrelease submunitions (CERS) warhead | Directed energy warhead | CERS and directedenergy design and development |
| Control Systems | Not available | Advanced actuator control system | Adaptive learning control system for maneuvering threats | Fast response controllers; innovative learning algorithms |
| Structures | THAAD | Composite airframe with integrated plumbing, wiring, and DACS | Composite advanced materials airframe with integrated plumbing, wiring, and DACS | Advanced materials; improved manufacturing techniques |
| Power | PAC3/THAAD/ ASAT batteries | Long life (60 min), high current density, lightweight | Long life (120 min), high current density, lightweight | Improved materials, packaging, thermal management |
parameters, data to develop engineering models, and computational fluid dynamics (CFD) validation data. AIT provides significant technology advancements in the seeker, cooled window/forebody, and high performance solid DACS. AIT has a variety of multiservice applications of risk reduction opportunities and performance enhancements (P3I). [POC: Mike Cantrell, (205) 9555968, email: cantrellm@smdc.army.mil]
The current technology capabilities, projected capabilities for 2009 and 1015, and innovations needed to achieve these capabilities are listed in Table D5.
Table D5. Endoatmospheric Interceptor Technology Plan |
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Component |
Today |
2009 |
2015 |
Innovations Needed |
| Polyacrylonitrile (PAN) Fiber | Conventional Japanese fibers, 55 msi modulus, 650 ksi tensile strength | Advanced composite fiber, 90 msi modulus, 800 ksi tensile strength | Advanced composite fiber, 100 msi modulus, 1000 ksi tensile strength | Research, improved materials development |
| Control Systems | None available | Advanced actuator control system | Adaptive learning control system for maneuvering threats | Fast response controllers; innovative learning algorithms |
| Structures | THAAD | Composite airframe with integrated plumbing, wiring, and DACS | Composite advanced materials airframe with integrated plumbing, wiring, and DACS | Advanced materials; improved manufacturing techniques |
| MMW Radomes | PAC3 | Dual mode RF/IR radome | Dual mode RF/IR, actively cooled, high strength/erosion resistance | Advanced materials development; improved manufacturing and characterization techniques |
| MMW Transmitters | PAC3/THAAD | 200300 W average, 4.5 kg, 150 inch2 | 200300 W average, 3.5 kg, 125 inch2 | Improved components, power generation and management techniques |
| MMW Antennas | PAC3/THAAD | Active conformal array | Active conformal array, dualmode antenna/aperture | Improved manufacturing |
| Algorithms | Basic discrimination algorithms | Onboard active/passive discrimination, control system algorithms for maneuvering threats | Algorithms promoting autonomous launch and forget operation | Improved S/D processors |
| IMUS | Army LEAP IMU, 0.4kg IFOG with 4deg/hr bias stability, 10mG acceleration sensitivity | 0.5kg RFOG with 0.01deg/hr bias stability, 100mG acceleration sensitivity, high bandwidth (5x existing) | Chip gyroscopes and accelerometers 0.01deg/hr bias stability, 100mG acceleration sensitivity, high bandwidth (5x existing) | Low loss fibers;
low loss optical connectors Improved laser source; improved micromechanical fabrication techniques Solidstate accelerometers Improved power management technology |
| Power | PAC3/THAAD | High current density, lightweight | High current density, lightweight | Improved materials, packaging, thermal management |
ShortRange Air Defense (SHORAD) With Optimized Radar Distribution (SWORD). The SWORD advanced technology program will provide the Army with mobile, allweather, closein defense against cruise missiles and shortrange ballistic missiles (SRBMs). Also, this system has capability against shortrange rockets, airtoground missiles, and UAVs. This program will leverage an interferometric radar and gigahertz (GHz) signal/data fusion technologies, utilize existing infrastructure, and achieve point and area defense performance exceeding existing fielded capabilities.
The SWORD concept was conceived from a BMDO initiative for NMD point defense. An interferometric fire control radar capable of command guiding an HTK interceptor to impact a strategic ballistic missile warhead out to a range of 25 km was initiated in early 1991. A 10meter (m) baseline Xband interferometric fire control radar and radio frequency (RF) transceiver was developed and demonstrated to perform this mission. This technology has demonstrated eight microradian angular accuracy at a 25km range. A tactical version of this system can be deployed on wheeled or tracked vehicles operating with a 23m baseline interferometric fire control radar. Specific advantages of SWORD include radar classification of hostile targets at ranges to perform intercepts at 10 km with optimized fusing, aimpoint, flight path, and divert firing techniques; providing 360degree search/track, onthemove (OTM) capability at 20 km; tracking 80 simultaneous targets; and controlling up to 5 intercepts every second. The estimated production cost goal of the missile is less than $15,000 and $8 million for the interferometric fire control radar. [POC: Ron Smith, (205) 9551182, email: smithr@smdc.army.mil]
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