One of the few accounts of INS Chakra, Charlie class submarine, in Indian service.
It may be recalled that Captain Alexander Ivanovich Terenov, the Russian safety captain of the Project 670 K-43 nuclear submarine INS Chakra from 1986 to 1991, who initially trained the Indian crews at Vladivostok, and then served alongside the three successive Indian captains for four years, has praised the Indian submariners for their professionalism in his book, “Under Three Flags, The Saga of the Submarine Cruiser K43/Chakra.”
The nuclear propelled Charlie was taken on a three year lease from 1988 from the Soviet Union. The deal was facilitated by Admiral of the Fleet Sergie Gorshkov, who was impressed by the Indian Navy’s Styx missile attacks off Karachi in the 1971 war and employment of Soviet supplied warships and submarines.
He reposed confidence that the Indian Navy could operate nuclear submarines effectively. The then Prime Minister, Mrs Indira Gandhi, had initiated discussions with Soviet leaders for leasing a nuclear submarine.
The Indian crew under Captain Ravi Ganesh took over the K-43 and named her INS Chakra. Around then, US President Ronald Reagan asked Moscow not to transfer the boat. The crew had completed training by December 1987, but was kept waiting in Vladivostok and not allowed to go on board for some time.
The book indicates that it was Prime Minister Rajiv Gandhi who then managed to swing the transfer by approaching President Mikhail Gorbachev. The submarine was hurriedly commissioned and christened INS Chakra by T.N. Kaul, India’s Ambassador to Russia, who hosted a lunch and sailed out of Vladivostok on January 5, 1988 when the temperature was minus 25 degrees C.
The Chakra was ordered by NHQ to dive and proceed till the Malacca Straits underwater to avoid detection. Jane’s Defence weekly photographed her off Singapore from where a naval warship escorted her to home waters. On February 3, 1988, Rajiv Gandhi personally embarked the INS Chakra off Vishakapatnam to welcome her into the Indian fleet.
The submarine dived, and the PM and his entourage had lunch with the Officers and the Coxswain, an important key senior sailor whilst under nuclear power underwater. The Indian crew handled the reactor well after the Russians put the officers and sailors through the paces of nuclear operation. INS Chakra was operated for 72,000 nautical miles (133,000km), and her reactor was active for 430 days.
Five missile and 42 torpedo firings were executed under the Indian command with Russian supervision on board for safety, which speaks volumes of operational capabilities over four years.
An accident and fire on board the Chakra in 1989 saw her lose electric power and descend from 40 feet to 200 feet. The crew expeditiously ordered ‘emergency blowing of the tanks’ to surface the boat. The fire was contained and put off by joint heroic action of the Indian crew and the few Russians on board including Terenov. There was no radioactive leakage and the submarine returned to Vishakapatnam on her own, possibly under diesel power, or with assistance of tugs as the reactor must have been scrammed (emergency shut). A Russian support team and the naval dockyard took three months to put her back to the sea.
Submarine accidents nonetheless have happened worldwide including in the US, UK and, the Soviet Navies; each equipped with major submarine arms. There are lessons to draw from them.
It would be imperative for the Indian Navy to examine the cause/s of all submarine accidents– technical or human failures– and do the needful as preventive measures.
http://indiastrategic.in/topstories3022_The_Indian_Navys_Submarine_Arm_is_Dependable.htm
Press Information Bureau
Government of India
Ministry of Defence
05-August-2013 18:47 IST
Mirage Aircraft
4.67% of the annual revenue expenditure is budgeted for spares and maintenance for the Mirage aircraft to maintain their required serviceability.
The prices of spares of Mirage-2000 aircraft are derived from Last Purchase Price / Price Catalogue escalated to current financial year. These prices are negotiated with the vendor every time through Contract Negotiation Committee meetings as per Defence Procurement Manual
The details of expenses during 2012-13 for the upkeep of the Mirage aircraft are as under:
Item
| width: 500 |
|---|
| [tr] |
| [td]Expenditure[/td] |
| [td](Rs. in Crores)[/td] |
| [/tr] |
| [tr] |
| [td]Procurement of spares[/td] |
| [td]228.00 = $44.7 mil[/td] |
| [/tr] |
| [tr] |
| [td]Repair of aggregates[/td] |
| [td]191.00 = $37.45 mil[/td] |
| [/tr] |
| [tr] |
| [td]Capital procurement[/td] |
| [td]61.16 = $11.99 mil[/td] |
| [/tr] |
| [tr] |
| [td]Capital Repair[/td] |
| [td]6.69 = $1.31 mil[/td] |
| [/tr] |
| [tr] |
| [td]Total[/td] |
| [td]486.85 = $95.46 mil[/td] |
| [/tr] |
Additional Agreement No.8 (AA 8), regarding new price escalation formula for supply of Mirage spares from Original EquipmentManufacturer (OEM) is under finalisation.
This information was given by Defence Minister Shri AK Antony in a written reply to Shri Kalikesh N. Singh Deo in Lok Sabha today.
http://pib.nic.in/newsite/PrintRelease.aspx?relid=97687
Average dollar to rupee rate 2012: $1= Rs51
The number of mirage in inventory to calculate operating costs = 49
Estimated flying hours ~ 200+
-> R&M budget of Mirage-2000 per plane per year ~ $1.94 million
Thank you for the info. So if 20 years ago it was a valid option for one missile, and it took that long before another missile of similar class entered service, it couldn’t have been because of technical hurdles but because of design choice. If IIR homing was best homing for most missons, we would have seen it proliferate on many more missiles. There are probably pros and cons to active and passive homing which is why even some of tomorrow’s high tech antiship missiles are planned with active radar seekers.
The processing power and algorithms required for IIR homing at such high velocities of relative motion would be a significant uphill task in sea skimming mode. For a maneuvering missile where the target might or might not always be in field of view it would be even more difficult to constantly co relate the seeker data with pre loaded target data.
Possible follow on version of Sudarshan precision guidance kit with GPS aided navigation. This variant looks significantly different from the current design and features mid course guidance. It carries laser gimbal in the nose and GPS and INS guidance unit in tail.
PG Kit for HSLD Bomb
The aim of PG kit is to convert dumb bomb in to a precision strike weapon which increases range of weapon manifold by aerodynamics manoeuvering. The kit is in the form of tail cone and nose cone and can be fitted easily around the bomb body. The tail cone houses mainly electromechanical fin actuation system, INS-GPS module, and a guidance on-board computer. The nose cone comprises of laser seeker module along with electronics.
Flight Control and Interface Electronics Unit
The purpose of flight control and interface electronics unit (FCIEU) is to implement guidance, navigation and control algorithms, interface with aircraft and GPS/INS unit, and issue control surface deflection commands to ACEU. It is required for real-time computing and sufficient I/O capabilities. FCIEU integrates with navigation sensors and implements three-loop autopilots and the trajectory control guidance algorithm. It implements the algorithms, which are computationally intensive and will have constraints of three-loop response time of few millisecond. Unit is also responsible for communicating with all sub-systems with pre-defined protocols on different serial interfaces. It has power source and regulation unit which generates different voltages required by different components on FCIEU and GPS/INS integrated module.
Salient Features
-Interfaces with USB memory for reading mission data
-Interfaces with aircraft over data bus for mission data reading and INS initialisation/ alignment
-Senses the release of the bomb from the aircraft and after pre-defined delay initiates the thermal battery
-Sends control signal to RF switch for correct GPS antenna selection
-Interface with GPS/INS unit for control and navigation Implements guidance and control laws (roll and lateral autopilots)
-Interfaces with ACEU for tail fin control
-Transfers laser code to homing head
-Sends start of scan command to homing head
-Interfaces with homing head for getting line-ofsight (LOS) rate
-Senses impact event/proximity and issue warhead initiation command
AMCA has been stalled since late 2012. All this wishful thinking that it will ever fly.
Zero confirmation on it. There is only one report about the project being put on hold from the Indian Express group and no other media outlet has confirmed on it, from official sources the program is entering full scale engineering design phase early next year. There is considerable research going on both in house and at university level wrt to AMCA technologies (RAOT materials, conformal antenna arrays, FBL, GaN t/r modules). All the updates about AMCA have come around Aero India events held every two years, it’s a nascent project, do not expect updates every other month.
Hence (imho) it is highly unlikely that the Su-30MKI can accommodate 2 of the 2.5T BrahMos’ and would explain the strengthening of the MKI airframe for the centreline pylon to accommodate it:

They shifted from single pylon installation to installation on tandem hardpoints in center line. Even if the hardpoints are mechanically capable of loading, the vibration and drag would play havoc with the structural integrity because of the size of the missile.

Isn’t AMCA stalled anyhow?
Nope.
With India’s economy coming to a crunch, I don’t think they’ll be pumping too much money into AMCA just yet.
Still doing better than a lot of countries.
An update on AEW&C program.
A couple of years back it was reported in a market study AESA module manufacturer about an AESA radar developed in association with CABS (centre for air borne systems) somewhere around 2010:-
http://crisil.com/capital-markets/CRISIL-Research_ier-report-astra-microwave-2012.pdf
S-band Active Aperture Array of 1244 elements using 100W TR modules
From DRDO Techfocus April issue on Radars, about L-Star program which is the ground based test bed for AEW&C array:-
http://drdo.gov.in/drdo/pub/techfocus/2013/TF_April_2013_WEB.pdf
New technologies for 200 W transmit receive modules, active array antennas, distributed beam steering network and digital receiver/Exciter have been developed and demonstrated.
Looks like the power output has been doubled in three years. Let’s hope that the APU and the power system on board was designed keeping these developments in mind.
Rare pictures of Remora EW Pod in Indian service.

As far as I know, these are the first and only pictures of IAF Mirage-2000s carrying the R-73’s APU-73 pylons. While it has been known for some time that the R-73 had been integrated with the IAF’s Mirage-2000s, there was no photographic evidence of it that I was aware of. Until now that is.
Definitely looks like it.

Coast guard wants upto 19 aircraft.
http://drdo.gov.in/drdo/tenders/viewTender.jsp?paramMicro=4924
Center for Airborne Systems (CABS) is involved with the Design and
Development of Multi-Mission Maritime Aircraft (MMMA) for Indian Coast Guard
(ICG). The envisaged MMMA will have the following roles:
‰ Maritime Surveillance and Interdiction
‰ Search and Rescue (SAR)
‰ Cargo and Personnel Transportation
‰ Air Ambulance
‰ Pollution Surveillance
For carrying out these roles various surveillance sensors, Pollution Sensors,
Gun etc needs to be mounted on a suitable modified aircraft for above
mentioned maritime roles. The various sensors will be integrated by CABS on a
suitable platform. The vendors are required to provide the availability of suitable
modified platforms towards this effort, along with willingness to carry out further
minor modifications according to the requirements of CABS and airworthiness
certification of the aircraft (with dummy loads and CFE’s provided by CABS).
The aircraft proposed by the vendor shall also be re-configurable for different
roles.
The earlier requirement was for 6 aircraft, the procurement for which was cancelled.
After a few hiccups during the pre-launch count down and even after the auto-launch, the 17-metre tall missile rose majestically from a mobile launcher and zoomed into the sky. After the three stages got separated as planned at different altitudes, the nose cone carrying the dummy payload withstood scorching temperatures of 3000 degrees celsius , while re-entering the atmosphere and zeroed in on to the pre-designated target point in the Indian Ocean, 5000 km away with an accuracy of a few metres after a flight duration of little over 20 minutes.

In ‘coming soon’ category, the Astra BVRAAM program.
is is possible.
look t this picture of a RMAF Su-30MKM, armed an AIM-120.
Obvious size mismatch.