Whenever
there emerges a cocktail made up of a notoriously trigger-happy bunch of
Italian state prosecutors, pathetic Indian politicians—both those in power and
those voted out of power—so full of unconscionable behavior, a cabal of
unscrupulous Italian citizens masquerading as product marketers, and
hyper-ventilating Indian broadcast TV channels, the end-result can only be
mayhem and obfuscation, with the truth nowhere in sight. On February 14, 2013 India’s
Ministry of Defence (MoD) had produced a document that—had anyone bothered to
read it—most notably the Italian magistrates—they would have indisputably
cleared all Indian citizens of any wrongdoing by removing the motive for
corruption.
All
that the three-year trials process in Italy has produced so far is the
indictment and sentencing of Giuseppe Orsi,
former CEO Finmeccanica; and Bruno
Spagnolini, CEO of AgustaWestland. No material
evidence to date has come to light about any direct or indirect money-trail
that leads to any Indian official or politician, nor of any wrongdoing done by
anyone from either the MoD or the Indian Air Force (IAF). Worse, the material
evidence gathered from the alleged middlemen—Guido Ralph
Haschke, Carlo Gerosa and James
Christian
Michel—clearly show them to be groping in the dark and being totally
unaware of how exactly the MoD’s procurement-related decision-making process
works. For, had they have had even the slightest idea about who had the final
say in selecting the VVIP helicopters, they would have clearly mentioned the
post of Director of the Special Protection Group (SPG) as being the key and
most critical stakeholder of the VVIP helicopter selection process. Yet,
nowhere is the SPG’s Director mentioned in any piece of paper containing the
handwritten notations of these alleged middlemen. Nor is there any material
evidence of any money laundering exercise involving any financial institution.
It
was in August 1999 that the IAF, which is responsible for carrying out VVIP
communication taskings, had proposed the replacement of its then Mi-8T VVIP
helicopters of its Air HQ Communication Squadron due to severe operational constraints, such as the Mi-8T’s inability of to
operate at night and in adverse weather, inability to operate safely at places
in elevations beyond 2,000 metres, and the approaching end of their total
technical service lives (TTSL). Consequently, a global Request for Proposals (RFP) was issued in
March 2002 to which four OEMs—AgustaWestland, Eurocopter SA, Rosoboronexport
State Corp and Sikorsky Helicopters—responded. The IAF’s Technical Evaluation
Committee (TEC) subsequently shortlisted three helicopters and accordingly competitive
flight evaluations were conducted. Since AgustaWestland’s AW-101 was not
certified for operating at an altitude of 6,000 metres, it did not participate
in the flight evaluations. Russia’s Mi-172 could not comply with 7 mandatory
Operational Requirements (OR). After flight evaluations, only Eurocopter’s
EC-225 was found suitable for acquisition. On November 19, 2003
a meeting was taken by Brajesh Mishra, the then Principal Secretary-cum-National
Security Adviser (NSA) to the then Prime Minister Atal Behari Vajpayee on this
subject. In this meeting, Mishra had observed that his main concern was that
the framing of the mandatory ORs had led India effectively into a single vendor
situation. It was also noted that very rarely have India’s Presidents or Prime
Ministers have made visits to places involving flying at an altitude beyond 4,500
metres. In
the meeting it was therefore decided to make the mandatory OR for an operational
altitude 4,500 metres. The higher flying ceiling of 6,000 metres, and the
mandated internal cabin height of 1.8 metres could be made desirable ORs. Later, a letter dated
December 22, 2003 from Mishra to the then Chief of the Air Staff (CAS) of the
IAF, ACM Srinivasapuram Krishnaswamy, stating that it was unfortunate that neither PMO nor the
Special Protection Group (SPG) was consulted while framing these mandatory ORs.
Mishra suggested that the CAS and the Defence Secretary may jointly review the
matter to draw up realistic mandatory ORs satisfying operational, security and
convenience requirements of VVIPs, and also set in motion a fast-track process
for selection and acquisition of the replacement helicopters. In pursuance of this
directive, the ORs were deliberated at length between IAF, NSA, SPG and MoD
between March, 2005 to September, 2006 and the indicated changes were
incorporated. No
ambiguity is thus possible: the decision to lower the service ceiling
requirement was official and above-board. It was taken during a meeting chaired
by the PM’s Principal Secretary-cum-NSA, was followed up in writing with the IAF’s
CAS, and was reviewed by the then-Defence Secretary. Subsequently, the revised
ORs were deliberated at length for 18 months by the involved SPG and IAF
authorities before becoming effective, and were all included in the final RFP
document. The
acceptance of necessity (AON) for the procurement of 12 VVIP helicopters was
accorded by the MoD’s Defence Acquisition Council (DAC) under the ‘Buy’
category with 30% industrial offsets on January 3, 2006.
Next,
the RFP was issued to six OEMs on September 27, 2006. Three OEMs—Sikorsky
(S-92), AgustaWestland (AW-101) and Rosoboronexport (Mi-172 ) responded to the
RFP. Rosoboronexport
did not submit the mandated earnest money deposit and the Integrity Pact, along
with the Technical and Commercial Proposals (TCP). It had been made clear to Rosoboronexport
in February 2007 that this was a global tender and hence every contractual
clause would apply to all vendors without exception. As no Integrity Pact and
earnest money deposit were received from Rosoboronexport, the Mi-172’s TCP was
not accepted. Subsequently, a team comprising officials of the
IAF and SPG carried out Field
Evaluation Trials (FET) of the AW-101 in the UK and of the S-92 in the US from January
16, 2008 till February 19, 2008. The FET team submitted its report in April
2008 and recommended the AW-101 for service induction. The IAF’s own internal Staff
Evaluation Report (SER) concluded that the S-92 was non-compliant with respect
to four staff qualitative requirements (SQR)m these being the absence of a
missile approach warning system (MAWS), service ceiling of 4.5km, deficient
drift-down altitude, and deficient hover-out-of-ground-effect parameters. In
addition, the AW-101, unlike the S-92, featured a high tail-boom since it would
allow the VVIP’s motorised vehicles to come right next to the rear-ramp and not
expose the protected persons to a threat from anyone in the vicinity. The SER thus assessed AW-101 to be fully compliant
with all SQRs.
The Technical Oversight
Committee (TOC) constituted by the MoD on August 6, 2008 found that the FETs,
compliance to SQRs and selection of the competing OEMs were all done according
to the prescribed/mandated procedures. A Contract Negotiations Committee (CNC) was subsequently
constituted and it carried out negotiations with AgustaWestland between September
19, 2008 and January 21, 2009. While the CNC was progressing with negotiations,
the IAF recommended the inclusion of Traffic Collision Avoidance System
(TCAS-II) and Enhanced Ground Proximity Warning System (EGPWS) as additional
fitments for all 12 AW-101s, while the SPG recommended the inclusion of integral
MEDEVAC systems for 8 of the 12 VVIP helicopters. These additional equipment
were considered to be essential for safe and effective operation of the
helicopters in the VVIP transportation role. The CNC, thereafter, recommended contract
signature at a negotiated fixed-price of €556.262 million ($827 million), or Rs.3,550 crore. The draft contract was next submitted for approval by
the Cabinet Committee on National Security (CCNS) and was approved by the CCNS on
January 18, 2010. Consequently, the MoD inked the contract with AgustaWestland for
12 AW-101s each powered by three Rolls-Royce/Turbomeca RTM-322 engines on February 8, 2010.
The
AW-101 procurement contract included specific contractual provisions against
bribery and the use of undue influence. Article 22 of the contract dealt with
penalty for use of undue influence. This clause entitled the ‘Buyer’ to cancel
the contract with the ‘Seller’ and recover from it the amount of any loss
arising from such cancellations. Article 23 of the contract dealing with agents
and agency commission required the ‘Seller’ to confirm and declare that it had
not engaged any individual or firm, whether Indian or foreign, whosoever, to
intercede, facilitate or in any way to recommend to the Government of India or
any of its functionaries, whether officially or unofficially, to award of the contract
to the ‘Seller’ nor had any amount been paid, promised or intended to be paid
to any such individual or firm in respect of any such intercession,
facilitation or recommendation. This clause further entitled the ‘Buyer’ to
consider cancellation of the contract without any entitlement or compensation
to the ‘Seller’ who shall be liable to refund all payments made by the ‘Buyer’
in terms of the contract along with interest. In addition to the
above contractual provisions, Agusta Westland had signed an Integrity Pact with
the Government of India. The validity of this Integrity Pact is from the date
of its signing and extends up to five years or the complete execution of the
contract, whichever is later. Under the Integrity Pact, the ‘Seller’ OEM
committed itself to take all measures necessary to prevent corrupt practices,
unfair means and illegal activities during any stage of the bid or during any
pre-contract or post-contract stage. Any breach of the provisions of the
Integrity Pact entitled the ‘Buyer’ to take actions against the ‘Seller’ which
included forfeiture of the earnest money, performance bond, cancellation of the
contract without giving any compensation, recovery of all the sums already paid
with interest, cancellation of any other contracts with the bidder, and to
debar the bidder from entering into any bid from the Government of India for a
minimum period of five years, which may be extended.
By July 2012 IAF pilots began
AW-101-related flying conversion training in the UK, and the first AW-101 arrived at the Palam air base on December 20, 2012 while the second was
delivered on December 22 and the third on December 24, 2012. Earlier, in October 2012, the MoD’s Defence Secretary wrote to the
Ministry of External Affairs’ )MEA) Secretary (West) to take up the matter of
alleged corrupt practices related the the AW-101 procurement contract with the UK
in view of the alleged involvement of a British citizen (James Christian
Michel), and the fact that the contract was signed with UK-based AgustaWestland. In November 2012, the
MEA’s Secretary (West) replied to Defence Secretary, stating that “the UK
authorities (i.e. the UK Serious Fraud Office https://www.sfo.gov.uk/about-us/) were
waiting for the results of the Italian investigation in order to ascertain
whether there are further actions to take”.
However,
by late 2013 Indian Defence Minister Arackaparambil Kurien Antony single-handedly took the decision to first block progress-payments
to AgustaWestland, then to cancel the contract, and finally to sue for payment
of the surety and performance bonds that the company had placed in escrow, on
the basis of unproven allegations. In doing so, Antony ignored a fundamental legal and
moral principle: that the accused is innocent until proven guilty. This is
unconscionable behavior for a Union Cabinet Minister in “the world’s largest
democracy,” and can only be explained by motives other that a constitutional
duty to his mission. The reality is that Antony, as the upcoming general
election neared, even wanted to put AgustaWestland and Finmeccanica, its
corporate parent, on the government’s blacklist, until he was blocked by the Government of India’s Solicitor-General. By January 2014, the
MoD had cancelled the €566 million contract, as well as encashed €228 million of
AgustaWestland’s €278 million performance bond, which dented the OEM’s cash
position and that of its holding company Finmeccanica. All of this for no other reason than
an Indian minister’s overwhelming pre-occupation with his political future.
So,
what are the results of the Italian investigative efforts thus far? Firstly, they
have only ended up insulting the institution of the IAF. Secondly, they have
denied the much-needed replacement VVIP helicopters that are not only required for
flying India’s President, Vice-President and Prime Minister, but are also meant
for use by the country’s National Command Authority (NCA) in times of
emergencies. In addition, such helicopters are also required to be put at the
disposal of visiting foreign Heads of State/Government. Imagine such an
official guest refusing to fly on-board a Mi-17IV or Mi-17V-5—both of which
generally shunned by civilian VVIPs across the globe due to their deficient
flight-safety features.
Here is what India’s
Directorate General of Civil Aviation (DGCA) says about the Mi-17 family of
helicopters: “The MGB drives the hydraulic pumps. Hydraulic power is required for
the flying controls. The hydraulic system has OM-15 hydraulic oil. Hydraulic
System has a main and standby system. Both systems have independent tanks,
pumps, accumulators and pipelines. However, both the pipelines feed only a
single booster, which in turn moves the control surfaces. There are a total of
4 boosters in the system. One critical weakness in the system is that if there
is a leakage in the booster, there is a possibility of the entire oil from both
the main and the standby systems leaking out. The emergency procedure for a
total hydraulic failure is to have both pilots flying the aircraft in unison to
a landing. The Mi 17V-5, which is a military version of the Mi-17, is being
flown by the IAF and Border Security Force. As per the Flight Manual of this
aircraft, the crew is to abandon the aircraft in case of total hydraulic
failure. In case they cannot, then they have to resort to flying by both pilots
to land immediately. Therefore, the procedure given in the Mi-17’s Flight
Manual for total hydraulic does not inspire confidence in the pilots. All of
them feel that this aircraft cannot be flown with a total hydraulic failure. They
feel that this aircraft cannot even be taxied on ground with total hydraulic
failure.”
And
finally, to add
insult to injury, Italian state prosecutors will be the only characters in this
sorry story to escape unscathed.
So, if all those pathetic
politicians (both of the ruling national coalition and those of the UPA-1/2
coalitions) in Lutyens’ Delhi are indeed serious about seeking the truth while
ensuring that the prestige of the IAF and the survivability of India’s NCA are
assured, then they better take heed of how Taiwan had overcome a similar crisis
in the not-too-distant past. The details of this case are as follows:
On August 31, 1991 France and
Taiwan signed the ‘Bravo Contract’ to supply six Lafayette-class guided-missile
frigates (FFG) for a total of US$2.5 billion. The buyer of the FFGs was the
Plans Office of the Republic of China Navy (RoCN), acting on behalf Taiwan. The
FFGs were to be built by DCNS. Shortly thereafter, the authorities in Taiwan accused
the French state-owned ELF Aquitaine of having paid bribes through Thomson CSF
(now THALES Group) to persuade both French government and RoCN authorities to
approve the contract and launched an investigation. Taiwan initiated arbitration proceedings against DCNI during the second
half of 2010. The case was
eventually heard by the International Chamber of Commerce’s International Court
of Arbitration. The court found that THALES Group had violated the anti-corruption
terms of the contract and was therefore liable to repay all bribes, plus
associated interest and legal fees. THALES appealed, and the decision was
upheld by the Paris Court of Appeal, ordering THALES Group to pay compensation
to Taiwan in the amount of €630 million (US$913 million). The French government
and THALES Group announced the payment of the fine, with the French government
paying approximately 72.54%, or around €457 million, and THALES Group the
remainder.
The Rebuttals
The Comptroller and Auditor
General (CAG) had submitted a report on the acquisition of helicopters for Very
Very Important Persons (VVIPs) on August 13, 2013. The audit sought to examine
the process of acquisition of VVIP helicopters and its compliance with the
Defence Procurement Procedure (DPP), the prescribed procedure for procurement
in the defence services. The report can be read
here:
Key findings and recommendations of the
CAG in this report were obviously derived by officials who were not domain
experts. The findings/recommendations are detailed below as are their rebuttals:
Claim:
The
initial Request for Proposal (RFP) issued by the Ministry of Defence in 2002
mandated an altitude requirement of 6,000 metres. Only one helicopter, the EC-225
of Eurocopter met this requirement. The EH-101 helicopter (later renamed
AW-101) of AgustaWestland did not meet this requirement.
Fact: That’s because that
RFP was based on specifications that favoured only the EC-225 and the Mi-172.
In fact, the MoD had in 1999 estimated that the total acquisition cost of eight
VVIP transportation helicopters would be no more than Rs.793 crore, and this figure pertained to only the Mi-172 helicopter
that did not contain any customer-specified equipment. The MoD had obtained
such cost estimations from Pawan Hans Ltd, which had by then been operating the
Mi-172.
Claim: However, the
first RFP was cancelled due to the emergence of a single-vendor situation. In
the revised RFP in 2006, the altitude requirement was reduced to 4,500 metres,
and a cabin height requirement of 1.8 metres was introduced, making the AW-101
eligible, and the EC 225 ineligible. The
lowering of the altitude requirement was against the ORs of the procured
helicopters, especially in many areas of the north and north east of India. In
addition, the single-vendor situation remained even after lowering the altitude
requirement, because of which the AW-101 of AgustaWestland was selected.
Fact: Totally untrue. At a meeting of
the PMO on November 19, 2003, it was Brajesh Mishra who, acting upon the advice
of the SPG, directed that the desired VVIP helicopter’s service ceiling be
reduced from 6,000 metres (18,000 feet) to 4,500 metres or 14, 000 feet; that
the internal cabin be of the stand-up type, meaning a height increase from 1.4
metres to 1.8 metres; and an increase in the number of VVIP helicopters from 8
to 12. Thus, 3 (THREE) different deviations were sought from the PMO, and NOT
from IAF HQ. A letter to this effect was later drafted by Brajesh Mishra from
the PMO and this letter was dated December 22, 2003 and it was addressed to both IAF HQ and to
the SPG’s Director. As a result of this, from that day itself, the EC-225 got
disqualified since its cabin height was only 1.45 metres.
Insterad, from then on, three contenders remained in the fray, i.e. the Mi-172,
the S-92 and the AW-101, with the latter two having cabin heights of 1.82
metres.
Claim: The revised
SQRs in 2006 made competition more restrictive instead of making the procurement
procedures more broad-based to increase competition. The fresh RFP with revised
SQRs was issued to only 6 vendors as opposed to 11 in 2002.
Fact: This is
spectacularly ridiculous. Can anyone in the CAG or in this world ever explain
how a competitive evaluation process involving 12 contenders can guarantee a
far better deal than a competitive evaluation process involving 6 contenders? Can
even a single such precedence be sited from anywhere else in this world?
Claim: The Field
Evaluation Trial (FET) of the AW-101 was conducted on representative
helicopters and not the actual helicopter. The AW-101 was still at the
development stage at the time of the FET.
Fact: Totally wrong. The
AW-101, known earlier as the EH-101, has been available as a fully developed
and flight-certified helicopter since the 1990s. Furthermore, never in the
history of aviation has any aircraft or helicopter been developed from scratch
as a VVIP platform. Every VVIP helicopter flying today makes use of a platform that
was originally developed for either military/military utility usage and that
has been customised through customer-specified fitments. Similarly, when the
Indian Navy wanted to evaluate the contenders for its LRMR/ASW platform
requirements, it had to evaluate representative candidates like the Airbus A319MPA
and the Boeing P-8A Poseidon.
Claim: Although the
2006 RFP had laid down the necessity of carrying out the field evaluations in
India, they were conducted abroad. The
recommendation and assurance given by the IAF Chief (October 2007) to conduct
evaluation trials abroad lacked justification.
Fact: Necessity, yes; compulsory, no. Deviations
from this requirement have always been allowed over the past 16 years. For
i9nstance, field evaluations of VVIP transport aircraft like the Boeing BBJ and
Embraer EMB-135BJ Legacy
were all conducted abroad in the previous decade.
Claim: Given the low
utilisation levels of the existing fleet of helicopters, the MoD was not
justified in procuring four additional helicopters for VVIPs.
Fact: The existing Mi-8Ts had approached
the end of their TTSLs by 2005 itself and therefore could be used only
sparingly. Instead, most VVIP flying between 2005 and now has been done on
board the IAF’s Mi-17-IVs, 40 of which were bought early in the previous
decade.
Claim: The cost
benchmarked by the Contract Negotiation Committee was much higher than the
offered price, allowing no room for negotiation.
Hence, it provided no realistic basis for obtaining an assurance about a
reasonable cost procurement of AW -101.
Fact: The MoD’s benchmarked cost was
Rs.4,877.5 crore while AgustaWestland’s offer-price was Rs.3,966 crore, meaning
the former figure was 22.80% higher. The final negotiated figure was Rs. 3,550
crore. Therefore, to claim that there was no room for negotiations on the price
issue is blatantly false. Usually, the benchmarked cost has a 20% mark-up in
order to factor in various variables, such as the customisation of the platform
(through the incorporation of special fitments) and the quantum of spares-support
required for a finite period of time, like for a single year or for a
three-year period.
Other Slanderous Claims
The Milan Appellate Court’s judgment
concerning Indian citizens, which relies almost entirely on the testimony of Guido
Haschke, blandly states: “Ultimately, there are no elements of certainty to
affirm this beyond any reasonable doubt that the reduction in the operating
height was made contrary to the public (duty), and then (Air Chief) Marshal
Tyagi carried out specific acts contrary to his duty; it remains, anyway, the
wrongfulness of his conduct, for having offered to cooperate with AW in an
economic operation which prohibited all forms of mediation, and for having
received a large compensation in relation to its institutional activity.”
Now, either Italian
state prosecutors and court judges are spectacularly insane, or they are loathe
to do their homework. For instance, the date on which written directives to revise
the QRs were issued from the Indian PMO to IAF HQ was December 22, 2003 and at that time the IAF’s CAS was ACM Srinivasapuram Krishnaswamy.
ACM Shashindra Pal Tyagi took over as the 20th CAS
of the IAF only on December 31, 2004, and had retired on March 31, 2007. The competitive evaluations of the
two shortlisted contenders were done during the tenure of ACM Fali H Major,
while contract signature for Contract No. HQ/S96062/6/ASR was done when ACM P V Naik was the CAS. Furthermore,
if at all the Italian state prosecutors and the presiding Judge of the Milan
Appellate Court were to have done their homework on how exactly the
decision-making process works for military procurements, they surely wouldn’t have
targetted S P Tyagi. All they had to do was study this document:
It is evident from this document that the
primary decision-makers on all technical aspects of production
evaluations/shortlisting within IAF HQ are the VCAS and DCAS Branches, and not
the office of the CAS. The bulk of the work is done by the concerned Project
Director who reports to the DCAS Branch and the final call is taken by the VCAS
Branch. The only job then left for the CAS is to ENDORSE the recommendations
and conclusions. He does not have the authority to either revise or reverse
anything at this stage.
Then we have utterly
false canards being spread by the TIMESNow broadcast TV channel, such as ZAPPA
being a code-word. In reality, Zappa is the surname of Giorgio Zappa, the former CEO of Finmeccanica. Similarly,
this Channel has since claimed that AgustaWestland International Ltd (AWIL) is
not an OEM. In reality, AWIL is indeed the OEM whose helicopter manufacturing
facilities are located in Yeovil, Somerset
in the United Kingdom, where the IAF’s first three already-delivered AW-101s
were built. And just like AWIL, the Italy-based helicopter manufacturing
subsidiary of Finmeccanica SpA is known as AgustaWestland SpA, while the
facility based in The Netherlands is known as Agusta
Westland NV, Netherlands.
The
false canards being spread by TIMESNow can be viewed here:
https://www.youtube.com/watch?v=xQ7VL7Gh1j0
218 comments:
«Oldest ‹Older 201 – 218 of 218To JOYDEEP GHOSH & PIERRE ZORIN: Will reply to all your outstanding queries later today.
Dear Prasun,
Thanks for your comments.
Meanwhile please see the below link. It gives the current status of Saudi Arabia.
http://www.thehindu.com/opinion/op-ed/alls-not-well-in-the-kingdom/article8576703.ece?homepage=true
Please Comment.
Thanks
S.Senthil Kumar
Dear Prasun,
And saudi came out with mega VISION 2030 with Manufacturing as key for success.
http://www.arabnews.com/news/manufacturing-play-key-role-realizing-vision-2030
1. Do you think saudi will succeed in Manufacturing Industry by pushing China & Indian industry Down?.
2. Can Saudi overcome the current OIL & GEOPOLITICAL Game and Keep hold of citizen?
Please Comment.
Thanks
S.Senthil Kumar
Prasunda said-
Pierre in French stands for Peter. In Italian it is Pietro, while in Spanish it is Pedro.
Thanks Prasunda for the information, you are a CHALTA -FIRTA encyclopedia...
"... as the saying goes, if you really want to enjoy & relish life, then you must also be willing to see life in its most naked, brutal & hellish form. "
VERY TRUE...what you look at and experience AUTHENTICALLY WILL DISAPPEAR & DISSOLVE...
Have a NICE day...
Pierre Zorin, a French...hhmmm..What's a Frenchmen doing here!!!...uummm AHA, YES he must be the MIDDLEMAN for the French Dassault Rafale deal...DON'T WORRY I won't tell this to your friend Pariah-kar, as you lovingly call him, or he will be after you, he is actually looking for this middleman...it will be a SECRET between both of us, BUT you have to pay me...kya kare CORRUPTION everywhere..
It's understandable why you were pissed-off at your friend Pariah-kar but I don't understand why you were pissed-off at your other friend AKA....i think he didn't pay you WELL..so you are trying to TAKE-OFF his sarong...NAUGHTY NAUGHTY...:)
Dear Prasun,
http://www.theindependentbd.com/post/43467
Please give your opinion regarding "Hanging of Jaamat-Islami Chief in Nizami in Bangladesh".
1. Can we expect more ISIS type of killing in Bangladesh in near Future?
2. By Hanging war criminals, Democracy is gaining or Islamization is gaining in Bangladesh.
Please share your thoughts.
Thanks
S.Senthil Kumar
Dear Prasun
Was trying to search on induction of HAL Rudra MK IV (WSI) with the indian army. the hal website shows that the latter is being manufactured and news are there dtd circa 2013 metnioining hadning over 2/3 rudras to IAAC. Please inform if the rudra has been inducted or is still awaiting fitment of Helina.
thanks
kunal
@Anup
Why?
Isnt the Naval LCA being Built for that every purpose? Testing on SBTF is one thing, but Test conducted on from an aircraft carrier would be beneficial
Also PPL check this
http://indiatoday.intoday.in/story/agusta-exclusive-top-10-disclosures-made-by-christian-michel/1/665376.html
https://www.youtube.com/watch?v=hNPBYtJyfZo
I am unable to understand how on earth someone can forbid such basic experiment, and why India unable to do such basic experiments to prove affects of EM on Gravity.
Further, I done some little research about history of anti gravity, negative mass, dark matter and and quantum vacuum energy aka Zero point energy aka Dark Energy by Dirac Equation. But scientist just rubbish this things as one cant think of negative mass in physical sense.
https://www.youtube.com/watch?v=OCuaBmAzqek
https://www.youtube.com/watch?v=tR6UebCvFqE
https://www.youtube.com/watch?v=0DL-Xa1f3QI
Further this pdf also explained how the Dirac Sea and Equations is the explanation of Dark Energy and Dark Matter.
http://www.theorionproject.org/Energy.pdf
Sorry that is wrong PDF file, the correct one is this
https://www.google.co.in/url?sa=t&source=web&rct=j&url=http://www.theorionproject.org/en/documents/BeardenPrecursor.pdf&ved=0ahUKEwiE5dei89LMAhWRHY4KHcRdAHgQFggZMAA&usg=AFQjCNEq0oihLaQmtkelfv1FYB-F8gLqBg&sig2=XSc8Zm6zKZ3LiA_qoA0vAg
http://www.theneworionproject.org/en/solving_bearden.html
To ARPIT KANODIA: It is best to read the OFFICIAL reports of countries, like the UK's Project CONDIGN. In it, everything is explored & explained & it has the official stamp of approval. Here is a summary:
http://www.ufocasebook.com/pdf/projectcondign.pdf
And here you will find the downloadable report's volumes:
http://webarchive.nationalarchives.gov.uk/20121026065214/http://www.mod.uk/DefenceInternet/FreedomOfInformation/PublicationScheme/SearchPublicationScheme/UapInTheUkAirDefenceRegionExecutiveSummary.htm
To KUNAL: Only 2 Rudras were delivered in 2013--one to the IAF & 1 to the IA. Nothing else so far.
To ANUP: 1) I had written about it way back in 2011 or 2012 that the LCA (Navy) Mk.1 has to be flight-tested from an aircraft carrier until its main landing gear physically breaks apart, i.e. a controlled crash on the carrier's deck. Because only this will prove the structural integrity & fatigue limits of the main landing gear & this is how it is done all over the world. Obviously such tests cannot be conducted on a SBTF. 2) No RM from India has so far given any date for service-induction or delivery schedule of the S-400 LR-SAM.
To PIERRE ZORIN: Regarding the Shortfin Barracuda SSK for RAN, it remains to be seen how a conventionally-powered version of this submarine will function. The original design called for a PWR as the power provider. Secondly, conventionally-powered SSKs can't dive down to depths achievable with nuclear-powered boats. Cruising speeds while being submerged is also lesser for SSKs. In India's case, acquiring an all-new production-line for a new-design SSN is a financial impossibility. In comparison, it is far more cost-effective to make use of the same vendor eco-system created for the SSBN programme for the SSN project. And this is exactly what Russia has proposed to India, which will save India all the trouble & money reqd for certifying & validating an entirely new vendor eco-system that would have been reqd for a SSN of non-Russia origin. What it means is that the SSBN & SSN designs of the IN will both feature a high degree of equipment commonality.
Christian Michel's tell-all interview, in which he too makes several points that I had raised a week ago (!), including pointing the figure towards the industrial offsets component & the need to do forensic auditing of this component:
https://www.youtube.com/watch?v=_V8NGueVy9Y
Hi,
We are in discussion with US to make F-16 or F-18 in India.
As per Media report the price of F-35 will come down to 85 million USD in near future.
Why we are not going for F-35. If it is a useless plane Israelis wouldn't have opted for it.
Dear Prasun,
Current Bangladesh politics.
https://www.stratfor.com/geopolitical-diary/bangladeshs-history-will-haunt-its-future
Thanks
S.Senthil Kumar
Dear Prasun,
Another View about "CPEC".
http://atimes.com/2016/05/csc-for-south-china-sea-arent-the-scariest-letters-in-the-world-theyre-cpec/
Thanks
S.Senthil Kumar
Is there a plan B for MMRCA if the Agusta Westland noise makes the current government audit the entire Rafale deal? If the Rafale gets audited from step one, then that would mean that there is no guarantee for a timely or reasonable closure of such an investigation, which would inordinately delay the IAF's force modernization plans.
I think a reasonable alternative would be to buy new-build Mig-29 UPGs. Upgrades like AESA MMRs would come later since it is more important for the IAF to get planes in operational numbers than to keep dithering on missed opportunities. This plan would not stretch funding on creating new infrastructure assets, as the necessary assets are already available. The savings from doing this would allow greater focus on in-house, indigenous capabilities rather than spending all of the MoD's energy on the crazy rat race of trying to barely meet minimum force preparedness requirements.
Thanks Prasun for the very interesting article about a complex issue.
Just a question regarding the IAF structure. You related to a 2005 official document which depicts the VCAS and DCAS organization.
In your opinion is this organization still valid ? For instance, I am talking about the number of ACAS and their roles. Indeed, as you know it is difficult to obtain a clear picture of the IAF full structure.
Thanks in advance
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