29 December 2014

India's Quest for MIRV Technology - Analysis


Multiple Independent Targetable  Re-entry Vehicle (MIRV)

US is a nation is preoccupied with its national interests and priorities more than any country on this planet, and this singular protocol seems to have inspired China, to robust emulation. As a mark of its new found power status the Chinese seem to be everywhere in and around the Asia-Pacific region. This crusade of belligerence and posturing is redefining standard foreign policies processes of many countries, specifically India, Japan, South Korea, Taiwan, Philippines and Vietnam who seem to have certain levels of niggling region. China's has been progressively increasing its defense budget vis-a-vis development of sophisticated weapons and defense related equipment over the last few decades. The result is China has introduced an appalling assortment of arms of sundry magnitude, China is also on the cusp of deploying Multiple Independent Re-entry Vehicle (MIRV) on their ballistic missiles, a development that is likely to have profound and pervasive outcome for the region and beyond.

What is a MIRV?

 
US Minuteman III MIRV ICBM launch sequence: 1. The missile launches out of its silo by firing its first-stage boost motor (A). 2. About 60 seconds after launch, the 1st stage drops off and the second-stage motor (B) ignites. The missile shroud (E) is ejected. 3. About 120 seconds after launch, the third-stage motor (C) ignites and separates from the 2nd stage. 4. About 180 seconds after launch, third-stage thrust terminates and the post-boost vehicle (D) separates from the rocket. 5. The post-boost vehicle maneuvers itself and prepares for reentry vehicle (RV) deployment. 6. While the post-boost vehicle backs away, the RVs, decoys, and chaff are deployed (this may occur during ascent). 7. The RVs and chaff reenter the atmosphere at high speeds and are armed in flight. 8. The nuclear warheads detonate, either as air bursts or ground bursts.

The US during the whetting era of cold war developed a uniquely dangerous weapon able to strike anywhere in the Soviet Union at wanton. The missile an MIRV also carried decoys and chaffs to evade air defense systems. This new technology undermined the entire balance of power between the two superpowers and struck fear into hard hearts of Soviet citizens.

The military purpose of a MIRV:


  • Provides greater target damage for a given missile payload. 
  • A multiple independently targetable reentry vehicle (MIRV) warhead is a collection of nuclear weapons carried on a single intercontinental ballistic missile (ICBM) or a submarine-launched ballistic missile (SLBM). Using a MIRV warhead, a single launch can strike several targets, or fewer targets redundantly. 
  • With single warhead missiles, one missile must be launched for each target. By contrast with a MIRV warhead, the post-boost stage can dispense the warheads against multiple targets across a wider area. Theoretically at least, only a small portion of an adversary’s missile force would be necessary to completely eliminate one’s strategic deterrent.
  • MIRV is destabilizing force primarily because they give nations greater confidence to destroy the enemy's critical missile sites in a first strike action by launching multiple, lower yield warheads.
  • Reduces the effectiveness of an anti-ballistic missile system that relies on intercepting individual warheads. Thus, in both a military and economic sense, MIRVs render ABM systems less effective, as the costs of maintaining a workable defense against MIRVs would greatly increase, requiring multiple defensive missiles for each offensive one. 
  • Decoy reentry vehicles can be used alongside actual warheads to minimize the chances of the actual warheads being intercepted before they reach their targets.
Why India needs MIRVs?

Agni-5 is capable of launching 4-5 multiple warheads, whose yield is unknown. Although it is not clear if the government has gone ahead and cleared the developed of MIRV system, former head of India’s DRDO, V.K. Saraswat, noted that several Agni variants could eventually be developed with this capability. Development of MIRV technology is vital to India's National Security because of potential threats from hostile adversaries, besides it will strengthen its aspirations of a complete nuclear triad and lastly it compliments India's minimum nuclear deterrence policy. Pakistan’s aggressive postures and China’s belligerence toward India in the recent past necessitates such an indispensable step. The deployment of MIRV technology will quantifying India's nuclear deterrence and enhance defence preparedness

Can India develop the Technologies involved?

The building blocks from boosters to radars, seekers and sophisticated mission control centers are currently available. DRDO had been able to develop key Radio Frequency seeker technologies for missiles, it has since indigenously perfected this technology, and digital processing during the missile's boost, mid-course and terminal phase is based on DRDO’s own software. The RF and Infra Red seekers are meant for proximity and precision engagement of targets, and both these technologies are required for the anti-ballistic missile (ABM) capability apart from other missiles as well. India is working on a new seeker technology with other countries also. Today, India is able to design and develop RF seekers, and in about a year or so, it will be independent in this key technology. Coming years would see greater Indian investment in micro-electro mechanical systems (MEMS), nano-sensors, nano-materials and advanced information technology tools. Such advancements would be essential for creating reliable, robust and highly accurate systems like the MIRV. This technology would enhance India’s nuclear deterrence capabilities. 

Cutting-Edge Techs

Weapon Dispersion

Analyzing a ballistic trajectory is a simple physics problem, but there is big difference betweem analysis and implementation. Recording the necessary data, rapidly analyzing it, combined with ever changing variables, to determine the precise moment to release a warhead so that it hits a specific target 8-10 thousand miles away, is not a simple task. Therefore, dispersing nuclear warheads is another major technological challenge.

China developed a method for deploying multiple satellites under a contract with Motorola. The deployment method utilized a "smart dispenser" to place Iridium class communication satellites into orbit and the know-how was transferred from Lockheed Martin Corporation. Another auxiliary technology required is the availability of expendable perigee/apogee kick motors, these are small booster motors set to lift satellites into higher orbits. 

However, India had developed both these technologies locally much before the Chinese cloned it. The PSLV-C20 launch in February 2013 is very significant because for the first time 7 satellites were inserted into their precise orbits using an embedded System-on-Chip (SOC) method, and the same SOC methodology is used for Agni-5 to assist its accuracy during its guidance and terminal phases. A notable point is that ISRO and DRDO have tested this key MIRV prerequisite by stealth which had clear military implications.

Miniaturization 

Miniaturization of nuclear and thermonuclear weapons as has been obtained to fit the nose cone spatial shape of Agni missiles. Weapons design and testing has to be simulated in a virtual environment using Super Computers since actual testing stands frozen after Pokhran-II. It must be assumed that BARC scientists have achieved the level of miniaturization deemed adequate and suitable 20 KT fission warhead.

Re-entry Design

All missile launch planning begins with a set of requirements that has to be met to achieve mission objectives. The re-entry phase of a mission is no different. There is a very delicately balance of three, often competing, requirements:

  • Deceleration
  • Heating 
  • Accuracy of landing or impact
Modern ballistic trajectory nuclear weapon system delivery vehicles typically utilize slender sphere-cone geometries with multiple warheads on a single delivery bus. For a given warhead and associated arming device, the designer selects the re-entry vehicle base diameter and vehicle length, which effectively determines the cone half-angle. The nose bluntness ratio is then selected based on drag and heat transfer considerations. The delivery vehicle has to sustain high high aerodynamic stress (deceleration) and heating, hence it must be made of advance materials. Although the agencies have worked extensively on aero-thermal structure and thermal protection system designs over the past decade for both its space and missile programs, its effective use on MIRV platform is yet to be ascertained.

Other prerequisites

  • Robust guidance and control computers with adequate computational abilities to conduct complex maths
  • Develop advanced and accurate inertial guidance systems such as gyroscope and accelerometers for precise and decisive targeting.
Conclusion

It is evident from history that there exists a close concurrence between space and missile programs as was the case with both the Soviet Union and America. China and India have also pursued the same path. The interchangeability of several technologies between the two entities suit there sustained development, but the more pronounced beneficiary is undeniably the missile program. Though the Indian missile program has matured to world-class levels, it is mastering some of the above technologies that will make MIRV integration as a holistic deterrent system.

by Admin



28 December 2014

India's own Anti-Hacking Program



by Indrajit Majumdar

Firstly, there is nothing called "Hacker Free Computer Environment" in the context of any Operating System (OS) in use today. This however, does not imply that it is totally inconceivable to make our defence servers and other services hacker free. With the growing number of such incidences of Cyberwarfare / Cyberterrorism and the increasing challenges posed by innovations in convergence, keeping the network alive can be possible only with very stringent security measures designed, implemented and deployed. Any specific requirement for limiting access to services should be deliverable as part of a security policy and should address till-date and forecasted attacks

We will discuss three methods of making a client computer or server hack free which also includes the currently work-in-progress C-DAC/DRDO anti-hacking program, the remaining two are purely concepts of the authors.

The C-DAC/DRDO Anti-Hacking Program:


C-DAC an affiliated lab of DRDO has initiated a plan to develop a fully indigenous Indian OS in mid 2010 involving government institutes, agencies and the academia. The construct was to develop a new operating system (both client and server variants) from scratch which would remain immune and free from malicious activities. The highly active international hacker community have been penetrating and infesting India’s state owned servers and other quasi-government systems rather frequently in the the past few years. The estimation was to keep the API, compilers, intranet protocols, algorithims and standards of the OS secret in the notion that the hackers will not be able to penetrate the OS and run encrypted viruses, polymorphic or metamorphic code or other Trojans/Worms since the environment will be on a proprietary domain. This would keep the government systems insusceptible to malicious attacks unlike in other popular operating systems like Windows, iOS/Mac OS, UNIX, Linux or other such OS variants. 

The new environment will also ward off typical approaches in attacks on connected system visible outside the intranet using network enumeration (discovering information about the intended target), vulnerability analysis (identifying potential ways of attack) and exploitation (attempting to compromise the system by employing the vulnerabilities found through vulnerability analysis). The new environment will be resistant to virus, exposure scanning, brute force attacks, password cracking, packet analysis, spoofing, root-kit infiltration, Trojans & worms and keystroke logging.

Development, testing and implementation is planned to be completed within the next two years. Testing phase will involve implementation of new network technologies and protocols. C-DAC drawing from its large pool of resources and skill sets has developed a full-duplex grid computing high speed, high bandwidth low latency network for the PARAM series of super computers called PARAMnet. The technology involves non-blocking crossbar based architecture at 2.5 Gbps full duplex bandwidth per port and distributed schedulers, the added advantage of this system enables to configure the existing protocol for any network topology. However, this exclusive technology can be scaled and modified to meet the specific security requirements. 

The First Concept:


This author’s first concept involves the development of an independent Internet Protocol architecture. Let’s call it the X-Net to avoid any confusion with the current INTERNET conformation which the world is currently using of now. 

The X-Net system should be a hierarchical network divided into three basic layers - Core (Level 1), Distribution (Level 2), and Target (End-User Level). Depending on the type of connectivity required by the users, geographical presence and location, connectivity should be provided across the country. It should use a consortium of bandwidth providers since no single vendor has the geographical spread necessary for creating a pan India network and connecting under served areas, the interface and feature set should be in conformance with the new design.

The design proposal is as follows:

  • Develop a System Area Network that provides high bandwidth, low latency communication. This design is normally used to interconnect nodes within a distributed computer system, such as a cluster. These systems are members of a common administrative domain and are usually within close physical proximity. Development should also include seamless inter-connectivity and data transmission with connecting protocols and algorithms, drivers, applications, industry grade & open source components, high-performance interface cards and high-speed scalable hubs, switches and application services for clients. 
  • It should have very low error rates and it must scale under load. 
  • Compatible and maturational browsers and server software that recognizes the protocols and standards. 
  • Hardware which can implement these protocols and standards. 
  • Wireless connectivity technology on the X-Net system will need the allocation of separate bandwidth frequencies, accompanied with new wireless hardware and software standards. 
  • Incorporate encryption technology with new military strength algorithms with future proofing. 
  • Keep the technology away from prying eyes by making the configuration intentionally incompatible and not connectible to the Internet. 
  • Segregating the domain into a dual model which enables private or privilege access of sensitive and public domain access for the general public who can access data which is not sensitive in nature. 
The Second Concept:

This is the most simple, most cost-effective, most easy and most secure idea of anti-hacking process which can be implemented. The solution: Abstain from connecting any storage of sensitive data on the public domain or any network. Store sensitive data in offline storage systems. The work computers used for the purpose of research and development purposes should be offline. 


(Indrajit Majumdar is an avid Defence and Space enthusiast and this piece was written by him exclusively for Defence Guru India)






27 December 2014

IRNSS Satellite Navigation System: Explained



Introduction

Since the beginning of time, human beings have looked to the sky to determine their whereabouts. Traditionally, the Sun and the pattern of fixed stars have been their guides. But in the second millennium, constellations of man-made satellites have taken over as beacons to guide the way.

What is satellite navigation?

Using the fixed stars, you can determine your position anywhere on the Earth’s surface to within a few hundred meters provided the weather is fine. But navigation satellites can tell you where you are to the nearest few meters or better, whatever the weather. Enhanced instruments can even pinpoint the position of a stationary object to within a few centimeters by measuring the object’s position many thousands of times over several hours and then working out the average of the measurements. Sophisticated new receiver technology picks up signals transmitted by navigational satellites. The receiver technology is small enough to be incorporated into the electronics of a car or mobile phone, and all our lives are changing as a result.

A satellite navigation is a system of satellites that provide autonomous geo-spatial positioning with global or regional coverage. The signals also allow the electronic receivers to calculate the current local time to high precision, which allows time synchronisation. A satellite navigation system with global coverage may be termed a global navigation satellite system or GNSS.

American Global Positioning System (GPS) technology is widely available for vehicles and smartphones. GPS was originally developed in the United States for defense related applications, way back in the 1970s, GPS services became available to civilians in the 1990s. The technology is based on the user's receiver picking up precisely timed radio signals from orbiting satellites, and calculating its distance from each source. Since the signals also communicate the position of each satellite in its orbit, the device can combine the information to pinpoint the location of the user in three dimensions. The precise time signals from the constellation of satellites - 32 in total for GPS - can also provide accurate time and synchronization data for mobile phones and networks.

Some of the major Satellite Navigation Systems are the Global Positioning System (US), GLONASS (Russia), Galileo (Europe), Indian Regional Navigation Satellite System (IRNSS), Quasi-Zenith Satellite System (Japan), Doppler Orbitography and Radio-positioning Integrated by Satellite-DORIS (France) and BeiDou-2 (China).

Indian Regional Navigation Satellite System (IRNSS)


Satellite Navigation service is an emerging satellite based system with commercial and strategic applications. ISRO is committed to provide the satellite based Navigation services to meet the emerging demands of the Civil Aviation requirements and to meet the user requirements of the positioning, navigation and timing based on the independent satellite navigation system. To meet the Civil Aviation requirements, ISRO is working jointly with Airport Authority of India (AAI) in establishing the GPS Aided Geo Augmented Navigation (GAGAN) system. To meet the user requirements of the positioning, navigation and timing services based on the indigenous system, ISRO is establishing a regional satellite navigation system called Indian Regional Navigation Satellite System (IRNSS).

(a) GPS Aided GEO Augmented Navigation (GAGAN):


This is a Satellite Based Augmentation System (SBAS) implemented jointly with Airport Authority of India (AAI). The main objectives of GAGAN are to provide Satellite-based Navigation services with accuracy and integrity required for civil aviation applications and to provide better Air Traffic Management over Indian Airspace. The system will be interoperable with other international SBAS systems and provide seamless navigation across regional boundaries. The GAGAN Signal-In-Space (SIS) is available through GSAT-8 and GSAT-10.

(b) Indian Regional Navigation Satellite System (IRNSS)

This is an independent Indian Satellite based positioning system for critical National applications. The main objective is to provide Reliable Position, Navigation and Timing services over India and its neighbourhood, to provide fairly good accuracy to the user.

IRNSS will provide basically two types of services:


  • Standard Positioning Service (SPS)
  • Restricted Service (RS) 

Space Segment consists of seven satellites, three satellites in GEO stationary orbit (GEO) and four satellites in Geo Synchronous Orbit (GSO) orbit with inclination of 29° to the equatorial plane. All the satellites will be visible at all times in the Indian region. The first satellite is scheduled to be launched in 2013 and the total seven satellite constellation is scheduled to be in place by 2016. Ground Segment is responsible for the maintenance and operation of the IRNSS constellation. It provides the monitoring of the constellation status, computation of the orbital and clock parameters and navigation data uploading. The Ground segment comprises of TTC & Uplinking Stations, Spacecraft Control Centre, IRNSS Timing Centre, CDMA Ranging Stations, Navigation Control Centre and Data Communication Links. Space segment is compatible with single frequency receiver for Standard Positioning Service (SPS), dual frequency receiver for both SPS & RS service and a multi mode receiver compatible with other GNSS providers.

Some applications of IRNSS are:

  • Terrestrial, Aerial and Marine Navigation 
  • Disaster Management 
  • Vehicle tracking and fleet management 
  • Integration with mobile phones 
  • Precise Timing 
  • Mapping and Geodetic Data Capture 
  • Terrestrial navigation aid for hikers and travellers 
  • Visual and voice navigation for drivers
Courtesy of IDN



25 December 2014

DRDO looks back on Year 2014


DRDO Tests Glide Bomb Successfully

December, 2014



A 1,000-kg glide bomb designed and developed by the Defence Research and Development Organisation (DRDO) was successfully tested in the Bay of Bengal off the Odisha coast. The bomb was dropped by an Indian Air Force aircraft.

Defence sources said the bomb, guided by its onboard navigation system, glided for nearly 100 km before hitting the target with precision. Its flight was monitored by radars and electro-optic systems stationed at the Chandipur-Based Integrated Test Range.

22 December 2014

Why GSLV MK-III success matters?


India's Crew Module Atmospheric Re-entry Experiment (CARE) flew to an altitude of 78 miles (126 km). CARE then separated from the upper stage of the GSLV Mk-III rocket, and landed over Bay of Bengal on Dec. 18, 2014

Significance of GSLV MK-III

  • It is the most capable rocket ever developed by India. It can carry up to 10 metric tons, or about 22,000 pounds, of cargo into low Earth orbit and up to 4 metric tons or about 8,800 pounds into geostationary transfer orbit once it is operational.
  • Validated complex atmospheric ascent regime, especially aerodynamic and control features that cannot be conclusively tested on ground.
  • Validated new design features which includes both Hardware and Software implementation
  • Performance validation of S200 solid boosters which generate 1.1 million pounds of thrust, making them the second-most powerful solid-fueled rocket motors currently in service after the strap-on rockets used by Europe’s Ariane 5 launcher.
  • Successfully tested 2 liquid-fueled L110 clustered Vikas engines using hydrazine as fuel which ignited when the rocket is already in the air, firing for more than three minutes and ramping up to peak power of 360,000 pounds of thrust. This is the first time ISRO has tested a clustered engine configuration.
  • The launch marked the successful testing of the atmospheric re-entry of a crew module, which separated from the rocket 325 seconds after lift-off at an altitude of 126 km, and descended in ballistic mode, re-entering the Earth’s atmosphere (about 80 km above sea level) and splashing down into the Bay of Bengal.
  • 1,600 degrees Celsius is the temperature that the CARE module withstood at re-entry into atmosphere, advanced heat shield technology was employed, further analysis of the data will reveal the actual temperature signature prevalent during re-entry phase.
  • Re-entry capability is key to sending a human into space. This is a complicated and dangerous manoeuvre; it is while re-entering the Earth’s atmosphere that the space shuttle Columbia was destroyed in 2003, killing seven astronauts, including Indian American Kalpana Chawla.
  • Finally, the global space industry is worth more than $ 300 billion, apart from the regular PSLV business and India has the potential to tap a substantial portion of this large pie once the GSLV matures as a reliable & credible launch platform.

17 December 2014

Major Achievements of ISRO Year Ended 2014



Introduction

The Indian Space Programme had a modest beginning with the launch of the first sounding rockets in November 1963 from the Thumba Equatorial Rocket Launching Station (TERLS), an obscure fishing village near Thiruvananthapuram for the investigation of ionosphere using sounding rockets. The primary objective of the Indian Space Program is to achieve self-reliance in Space Technology and to evolve application program to meet the developmental needs of the country, thus ISRO was brought under the newly formed DOS in September 1972. 

Since then, over the last five decades, the ever challenging task of space technology development and utilisation, has not only graduated from experimental and demonstration phases to an operation era, but also provided its potential to address the national needs. Notable progress has been made in the design, development and operation of space systems, as well as, using them for vital services like telecommunications, television broadcasting, meteorology, disaster management support and natural resources survey and management including climate variability and change.