Archive for the ‘Technology’ Category

Was it biological or nuclear materials on X-37B?

October 18, 2014

The technicians servicing the  X-37B spaceplane shortly after the unpiloted craft glided to a computer-controlled landing Friday at Vandenberg Air Force Base are very well protected from something.

With Ebola protective suits in mind, their clothing would suggest the presence of nuclear or biological materials being on the spaceplane which has just returned from its 674 day secret mission.

They seem to be carrying their own completely isolated environment.

Technicians service an X-37B spaceplane shortly after the unpiloted craft glided to a computer-controlled landing Friday at Vandenberg Air Force Base, Calif., to close out a classified military mission, CBS/ U.S. AIR FORCE

ISRO successfully launches 3rd of the 7-satellite IRNSS

October 16, 2014

After the successful arrival of the MOM in Mars Orbit, ISRO has taken the more mundane step of putting the 3rd of 7 satellites for India’s satellite navigation system into place.

ISRO’s Polar Satellite Launch Vehicle, PSLV-C26, successfully launched IRNSS-1C, the third satellite in the Indian Regional Navigation Satellite System (IRNSS), in the early morning hours of today (October 16, 2014) at 0132 hours IST from Satish Dhawan Space Centre, Sriharikota. This is the twenty seventh consecutively successful mission of PSLV. The ‘XL’ configuration of PSLV was used for this mission. Previously, the same configuration of the vehicle was successfully used six times.

The Indian Regional Navigation Satellite System (IRNSS) is India’s 7-satellite global positioning system. It is similar to the GPS of the US, Russia’s Glonass , Europe’s Galileo  China’s Beidou and the Japanese Quasi Zenith Satellite System. The IRNSS is autonomous and under the control of the Indian Government. In addition to providing civilian navigation services (Standard Positioning Service – SPS) in a region extending 1500 km beyond the country’s borders, the IRNSS will also provide encrypted military and strategic services (Restricted Services – RS) independent of foreign governments. The positioning accuracy is designed to be 20 m in the primary service area. Each satellite is designed for a life of 10 years.

The IRNSS program received government approval in 2006 and is planned to be fully deployed by the end of 2015. The budgeted cost is 14.2 billion INR (about $240 million) and must count as another example of ISRO’s “frugal engineering”. The cost includes for two stand-by satellites on the ground making nine included in the budget. As a comparison Europe’s Galileo navigational system comprises 27 satellites and is expected to cost about 50 times more at about €10 billion ($13 billion).

IRNSS - ISRO

IRNSS – ISRO

The 7 satellite system consists of 4 satellites as two pairs of geosynchronous satellites and 3 in geostationary orbit. The first two satellites in the series, IRNSS 1a and IRNSS 1b formed the first geosynchronous pair and were launched from Sriharikota on July 1st, 2013 and April 4th this year. respectively. The IRNSS-1c launched this morning is the first geostationary satellite and carries two payloads, one for transmitting navigation service signals to users and another consisting of a C-band transponder to facilitate Cube Retro Reflectors for laser ranging. It is the central satellite of the seven satellite configuration. The satellites launched so far are individually operational but the system will become operational only with the next launch of a geostationary satellite. (The system needs one geosynchronous pair, the central satellite and one more geostationary satellite to reach the threshold conditions to become operational). All seven satellites are planned to be in place and operational by the end of 2015.

IRNSS Architecture - ISRO

IRNSS Architecture – ISRO

NasaSpaceflight:

Based on ISRO’s I-1K satellite bus, each IRNSS satellite has a mass at launch of 1,425 kilograms (3,142 lb). Unfuelled, the spacecraft has a mass of only 600 kilograms (1,323 lb), with the remaining 825 kilograms (1,819 lb) being taken up by propellant for their apogee motors and manoeuvring engines.

The spacecraft are designed for ten years’ operational service. Generating 1.6 kilowatts of power through twin solar arrays, the satellites broadcast L5 and S band navigation signals. C-band transponders and retroreflectors are used for range calibration.

Each satellite is fitted with a single liquid apogee motor producing 440 newtons (99 pounds-force) of thrust. Three-axis control is provided by reaction wheels, magnetorquers and twelve reaction control thrusters.

The apogee motor is tasked with propelling the satellite from its initial deployment orbit into the final geostationary orbit, while the remaining thrusters will be used to manoeuvre and orient the spacecraft once it is in orbit.

IRNSS-1C is the first geostationary satellite in the IRNSS system. Planned for operation at a longitude of 83 degrees East, it will operate at the middle station of the constellation.

Two more geostationary satellites will be added; at longitudes of 34 and 132 degrees, while the remaining four spacecraft will operate in inclined geosynchronous orbits to increase the angle of separation between signals. Two of the inclined satellites are already in orbit; IRNSS-1A and 1B operate at a longitude of 55 degrees East. A second pair will be located at 111 degrees East next year.

The two satellites already in orbit were deployed in July 2013 and April 2014, both riding PSLV rockets to orbit from the Satish Dhawan Space Centre

The PSLV launch vehicle was introduced in 1993 and this is its 28th successful use (27th consecutive successful use). Today’s launch used the PSLV-XL configuration – the most powerful version of the PSLV currently flying – which makes use of six PS0M-XL boosters containing S-12 solid rocket motors. Four of these motors are lit when the rocket leaves its launch pad, with the remaining two lit during the early stages of its ascent.

 

MOM successfully enters Mars orbit – first time ever on a maiden Mars mission

September 24, 2014

In what appears to have been a remarkably flawless and precise operation ISRO’s MOM has entered Mars orbit. It is the first time that a country has succeeded to get a spacecraft to enter Martian orbit on its maiden attempt.

“We have the signal.

1099 m/s.

Expected – 1098.7 m/s”

(The Mars Orbit Insertion burn had a planned duration of 24 minutes and 14 seconds, slowing the spacecraft down by 1,098.7 meters per second to be captured in an elliptical orbit around Mars.)

The operations took place while the spacecraft was behind Mars. It seemed an endless wait for it to reappear. It was then a seemingly endless 12.5 minutes from when telemetry was reactivated and the signals were received confirming that the maneuvers had been successful.

The precise orbit achieved now awaits further tracking information.

Foto

Prime Minister Narendra Modi arrived at ISRO in time to witness the critical and historical phases of the orbit insertion procedures (and he is to be highly commended for preferring real things to the meaningless, pointless and futile climate change talkshop at the UN).

He was more than a little pleased.

Narendra Modi at ISRO after MOM achieved orbit — screen grab by The Hindu

A major step not just for India’s confidence in its technological capabilities but also for its geopolitical positioning against China.

BBC: If all goes well and the satellite orbits the Red Planet, India’s space agency will become the fourth in the world after those of the United States, Russia and Europe to undertake a successful Mars mission. …..

…… After India’s successful unmanned Chandrayaan mission to the Moon in 2008 that brought back the first clinching evidence of the presence of water there, the Mars mission, according to K Radhakrishnan, chairman of the Indian Space Research Organisation (Isro), is a “natural progression”. …….

India sees the Mars mission as an opportunity to beat its regional rival China in reaching the planet, especially after a Russian mission carrying the first Chinese satellite to Mars failed in November 2011. Japan also failed in a similar effort in 1998.

China has beaten India in space in almost every aspect so far: it has rockets that can lift four times more weight than India’s, and in 2003, successfully launched its first human space flight which India has not yet embarked on. China launched its maiden mission to the Moon in 2007, ahead of India.

So if India’s mission succeeds, it will have something to feel proud about.

Culmination nears for India’s Mars Orbiter Mission

September 23, 2014

In 8 hours – if everything goes as planned – the MOM would have been inserted into Mars orbit of 423 km at periareion and 80,000 Kilometers at apoareion  at an inclination of 150 degrees and with an orbital period of a little more than three days. Though a number of experiments are planned, the most important objectives of the mission – to demonstrate technology and capability – will largely have been accomplished on getting into orbit.

Frugal engineering and with a cost of about 10% of that of NASA’s MAVEN will have taken ISRO’s MOM into Mars orbit – and at the first attempt.

But the next few hours will be tense and nervous not only for ISRO mission staff but for the many millions of Indians who will be following the live webcast at http://webcast.isro.gov.in/. The critical operations will take place while the MOM spacecraft is occluded on the far side of Mars and when signals will be taking over 12 minutes to reach earth.

Spaceflight101: 

The critical Mars Orbit Insertion Burn Sequence will begin three hours ahead of the planned maneuver time when the spacecraft automatically switches over to its Medium Gain Antenna for communications since the High Gain Antenna will be pointing away from Earth during the retrograde burn.
21 minutes ahead of ignition, the spacecraft will begin the re-orientation to the proper attitude for the burn, pointing LAM to the direction of travel. The re-orientation is accomplished using the vehicle’s Reaction Wheels. Five minutes and 13 seconds ahead of the burn, the spacecraft passes into darkness – for the first time since leaving Earth last year. In advance, MOM will fully charge its battery to be in a safe configuration for the eclipse.
Three minutes ahead of the burn, the vehicle’s eight 22-Newton thrusters are enabled to start providing attitude control which they will continue to do throughout the main engine burn, keeping MOM pointing forward. Ignition of the Liquid Apogee Motor is planned at 1:47:32 UTC on Wednesday, September 24, 7:17 Indian Standard Time. The Mars Orbit Insertion burn has a planned duration of 24 minutes and 14 seconds, slowing the spacecraft down by 1,098.7 meters per second to be captured in an elliptical orbit around Mars. During the burn, the engines will consume 249.5 Kilograms of propellant leaving only about 40 Kilograms of propellant for the rest of the mission.
Should something go wrong during the burn, MOM is programmed to react appropriately in order to achieve a stable orbit around Mars – even if that means to spend all the vehicle’s propellant to do so. In the event the Liquid Apogee Motor is not ignited or its burn is cut short, MOM would automatically switch to the 22-Newton thrusters to supply as much delta-v as possible. Due to their lower thrust, the 22N thrusters would need to fire much longer than LAM along a greater stretch around the periapsis pass which will increase propellant consumption and leave MOM in a higher orbit.
MOI timeline

Graphic ISRO (via spaceflight101)

MOM test fires liquid motor for orbit insertion on Wednesday

September 22, 2014

A sigh of relief today as the liquid fueled motor was successfully test fired for 4 seconds after having last been used 9 months ago.

The 440 Newton Liquid Apogee Motor (LAM) of India’s Mars Orbiter Spacecraft, last fired on December 01, 2013, was successfully fired for a duration of 3.968 seconds at 1430 hrs IST today (September 22, 2014). This operation of the spacecraft’s main liquid engine was also used for the spacecraft’s trajectory correction and changed its velocity by 2.18 metre/second. With this successful test firing, Mars Orbiter Insertion (MOI) operation of the spacecraft is scheduled to be performed on the morning of September 24, 2014 at 07:17:32 hrs IST by firing the LAM along with eight smaller liquid engines for a duration of about 24 minutes.

The MOM is now in (or just entering) Mars’ sphere of influence and is effectively falling freely towards Mars. The orbit insertion procedure is described here.

Mars Orbit Insertion for MAVEN and MOM

graphic: indiaspaceactivity

On 24th 0127 GMT, even as it is falling with speed of 4 kms/sec, the craft is reoriented so that the thrusters face forward  ( for the next orbit maneuver of retro thrust to reduce the speed and to direct it in the required orbit ). The re-orientation is completed @ 0147 GMT. MOM would by this time be falling with a speed of  4.48Km/sec.

After the disturbances due to reorientation have died, i.e. 5 seconds later,  the Retro action starts with the firing of  LAM using 8 thrusters ..  the fall speed by now is 4.68 km/s. Even as the thrusters start their effort to reduce the speed of MOM, the fallingspeed continues to increase due to the gathered momentum upto 5.89 km/s and thenspeed  starts falling. The LAM firing also directs the craft in the desired direction so that it achieves the required orbit around Mars. The LAM operation ends @0216GMT.

As shown in figure there the MOM speed would increase from 3.18 Kms/sec to 5.89Kms/sec @  0216GMT.

Now notice that MOM approached Mars parellel to  equator unlike MAVEN which approached over North pole.  The reason for these two approaches is that the final orbits of MAVEN and MOM are inclined @ 75 deg and @ 19 deg respectively. This is evident from the ‘ cross roads ‘ seen between MOM and MAVEN release in the combination diagram shown above.

In the above flow of sequence we did not have time to  mention a couple of more chilling facts: @ nearly the same time when LAM operation starts MOM would go behind Mars as seen from Earth. Secondly , even if it was visible, whatever happens at MOM will be known to Earth only after 12 minutes due to the distance between Earth and MOM. So all this (and next described operations ) are being done under the unsupervised pre-loaded command sequences. So the success indicates how well are we in anticipating the situation through modelling.

A detailed look at dynamics of acceleration during this critical operation is shown in this graphic. (numbers are in kms/sec/sec ) corrosponding to sky blue curve. (X axis is time axis from 0110GMT to 0310GMT of 24 Sep. )
Violet curve is the speed normalized to fit in this graph with that of acceleration. Actual speed variation shown corresponds to 3.88 km/sec at left to 5.89km/s at peak near center which falls to 4 km/s at lsft edge.

We have also marked the events of reorientation (between red dots) and retro rocket firing (between Green dots ) on acceleration curve.

Notice that the LAM retro action started at first green dot on left ( 0152 GMT ) ..  it has tried to reduce the speed but the fall is more powerful, so MOM speed continues to increase despite retro action. This continues and for sometime eventhough the acceleration has started reducing ( blue line coming down ), the gathered momentum  makes the craft to increase its speed for sometime. Finally however the thrusters succeed in reducing the speed ( reversal near center of violet line ) ..  the thrusters are also turned off at that moment.(green dot near the center of graph ). Now the total operation of MOI is over.

Incidentally, the point where speed reversal has taken space forms the lowest point near the surface of MOM prior to first perigee which would occur after the craft completes one revolution.

Oh Dear! Celebrities whinge at release of naked pictures

September 2, 2014

I am concerned that iCloud can be hacked – but only because my assessment of their security was clearly wrong. I’ll just have to give iCloud a lower rating for security than I have done.

But I cannot share the indignation of the celebrity “victims” at having their naked pictures publicised  and their “plight” leaves me largely unmoved.

The hackers may be despicable but those who upload naked pictures of themselves (or other compromising material) into the Cloud are just plain stupid. In fact I feel sure that the act in itself is some subconscious (or perhaps conscious) craving for the pictures to be leaked and for the resulting publicity. Stupid people can also be victims but my sympathy for stupidity is very heavily tempered.

What is much more upsetting is that I haven’t seen any of these pictures yet (but I shall not be spending any time looking for them either).

Ricky Gervais got it right first time.

Apparently he has now back-tracked somewhat in response to protest but I only think the less of him for that.

The comedian was criticised after posting this message on Twitter - blaming celebrities for taking the photos and storing them on their computers in the first place 

MOM and MAVEN approach Mars

August 12, 2014

Both the Indian Mars Orbiter Mission (MOM – Mangalyaan, budget $70 million) and NASA’s MAVEN (budget $672 million) are now approaching Mars. Both are doing well according to their latest status updates.

MOM was launched on 5th November last year and MAVEN on 18th November, 2013. Whereas MAVEN on its Atlas 5 rocket could directly enter into a  Hohmann Transfer Orbit with periapsis at Earth’s orbit and apoapsis at the distance of the orbit of Mars, MOM had to take the low-cost, scenic route. Because of the relatively low payload capability of the PSLV launch rocket, MOM had to spend 26 days in ever-increasing earth orbits. MOM had to fire its Liquid Motor six times to work its way up to departing Earth orbit using a standard Hohmann Transfer Orbit on 1st December.

Alternate paths to Mars: NASA’s MAVEN compared to India’s MOM

MAVEN - MOM trajectories

MAVEN – MOM trajectories

 

When they were launched MAVEN was expected to reach Mars on 22nd September 2014 and MOM 2 days later on 24th September 2014. The time lines have shifted slightly subsequent to the mid-course corrections carried out and MOM is now expected to reach Mars orbit about a week ahead of MAVEN. I suspect that the time of Mars Orbit Insertion is still a little fluid, but both are about 1 month away. MOM is currently about 6 minutes away in radio signal distance.

Discovery News:

India’s Mars Orbiter Mission (MOM) is more than 80 percent of the way to Mars and performing well, according to a Facebook update posted July 21 by the Indian Space Research Organization. MOM is expected to enter orbit on Sept. 14.

The second craft, NASA’s Mars Atmosphere and Volatile EvolutioN (MAVEN), is also performing well. MAVEN is scheduled to embark on its final approach to the Red Planet on Sept. 21, one week after MOM’s arrival, principal investigator Bruce Jakosky said. After months of checkouts and tests, the spacecraft will now be left quiet until close to the big day.

NASA’s MAVEN has now gone into a “pre-Mars Orbit Insertion moratorium.” All systems required for a safe Mars Orbit Insertion remain powered on. But other systems like the instruments are shut down until late September because they are not needed for a successful MOI. We want the spacecraft system to be as “quiet” as possible and in the safest condition during the critical event on September 21st”.

Related: Frugal engineering for India’s Mars mission

The end of the road for the large Alstom gas turbines?

July 7, 2014

(corrected February 2015)

The large (>50MW) Alstom gas turbines (GT11N2, GT13E2, GT24 and GT26) represent a line of technology which derives mainly from the BBC range of products (developed further as ABB) and acquired by Alstom in 1999. At that time Alstom’s licence with GE came to an end. But as GEC-Alsthom, Alstom had also inherited the gas turbine technology which came out of GEC in the UK. In the current Alstom range not much remains of the GEC tradition. At the smaller end Alstom also once had the gas turbine technology of the Ruston engines from Lincoln and acquired the ABB range of small machines (which themselves carried forward the developments as ASEA and some of the Sulzer range). But the entire range of industrial (<50MW) gas turbines was divested to Siemens in 2003 (and they are doing very well there).

Now as GE takes over Alstom’s power business (which has still to get final regulatory approval but looks to be a done deal), the days of the Alstom range of large gas turbines are strictly numbered. GE (and Siemens) have their own machines competing directly with the GT24 (60Hz) and GT26 (50Hz) and I do not expect that any more of these machines will ever be sold again. The sequential combustion design concept that these machines employ is so far from the GE approach that it seems impossible for any versions of these machines to continue. Alstom (as ABB) had adopted sequential combustion in the late 1990’s firstly to differentiate themselves from GE and Siemens and to get over their lack of access to advanced, high-temperature materials coming out of military jet engine programmes. Sequential combustion was first used/tested by BBC in the 1960’s 1948* though at much lower temperatures and ABB was trying to create a virtue out of a disadvantage – which the GT24 and GT26 did eventually do, but not without great problems and great cost.

GE may well have some benefit from some of the component solutions that Alstom has been forced to develop – at great expense – to get over the challenges posed by sequential combustion. Similarly some of the low-NOx solutions developed by Alstom could possibly be of use for GE. There may be some tricks for GE to pick-up regarding compressors. Certainly GE will continue with the very lucrative service market in maintaining the Alstom fleet and this will continue for perhaps 10 or 12 years at most. So while GE will benefit from the service revenue and by the reach of Alstom’s global sales organisation, the GT24 and GT26 – as products – have very little benefit to offer. It will not be possible for GE to absorb all the manpower currently employed with Alstom’s gas turbines. Not all those currently involved with the design and manufacture of the GT24 and GT26 will be needed for – or be able to switch over to – the design and manufacture of the GE range. GE’s global procurement network and its qualification of sub-suppliers is probably much more advanced than Alstom’s. I don’t expect that GE’s global sourcing will be much enhanced by the acquisition of Alstom’s Power business. Some job losses at Alstom locations are inevitable and I suspect these will be mainly in Switzerland while jobs in France will be somewhat protected by GE’s promises to the French government. At Belfort, Alstom produced GE machines under licence till 1999 and no doubt this will become GE’s centre for large gas turbines in Europe.

The GT11N2 gas turbine will probably die a natural death. It has not been a really competitive machine for over a decade and even though it has gone through many upgrades and cost reduction exercises, It has some unique advantages with low-Btu fuels but I do not think it offers GE any great advantages and they already have competing machines. The GT11N2 may have survived a little longer within the more restricted Siemens stable but even here it would have eventually withered.

The GT13E2 is possibly the only machine that may survive for a while under GE. It has some unique advantages with low-Btu fuels and could have a geographical market niche in Russia and the former CIS countries. But if it does survive it will do so only as a niche product. Again it would probably have had a longer life under Siemens but my guess is that it will not be sold for more than another 2 or 3 years.

The next market boom for large gas turbines – by my analysis – will come in the second half of 2015. This will be due partly to the 7-8 year “normal” business cycle and partly due to, and reinforced by, the advent of shale gas. And when that boom comes, the Alstom machines will be absent and there will be one less gas turbine technology available in the world. GE, Siemens and MHI will be the only three technologies left and they will be the main beneficiaries. But just three technologies are not enough. A growing market together with a dearth of technology suppliers will probably ensure the entry of another player into the field of large gas turbines.

(Actually Siemens and MHI get the best return at the lowest cost. They gain increased market space as Alstom’s machines disappear at no cost to themselves. GE gains no new products, gets the same increased market space and gets increased service revenue for Alstom machines. But GE has a large cost of acquisition and a great deal of hassle – and cost – to come as they restructure and integrate the Alstom business).

I would guess that this fourth player could well be Shanghai Electric with their newly acquired 40% stake in Ansaldo Energia. This has been something of a coup for Shanghai Electric. Doosan were also eyeing Ansaldo as a way of entering the gas turbine playing field (the entry barriers are too high for a scratch player). Both Doosan and Siemens had made bids for Ansaldo Energia but Siemens’ bid was essentially a defensive and a spoiling bid and they eventually withdrew. Doosan were the sole remaining bidder but it seems that Shanghai have pipped them at the post for this strategic acquisition.

* Correction – Sequential combustion was first used by BBC at Beznau in 1948, operating on distillate and with a TIT of 575ºC.

100 days to Mars for ISRO’s Mangalyaan

June 16, 2014

Four days ago

  • The second Trajectory Correction Manoeuvre (TCM-2) of India’s Mars Orbiter Spacecraft was successfully performed on June 11, 2014 at 1630 hrs IST. TCM-2 was performed by firing the spacecraft’s 22 Newton thrusters for a duration of 16 seconds.
  • At present, the radio distance between the Spacecraft and the Earth is 102 million km. A radio signal from the Earth to the Spacecraft now takes about 340 seconds. The spacecraft so far has traveled a distance of 466 million km as part of its total Journey of 680 million km.
  • ISRO is continuously monitoring Mars Orbiter Spacecraft using Indian Deep Space Network (IDSN). The spacecraft and its five scientific instruments are in good health.

And 100 days from today on 24th September, ISRO’s frugally engineered  Mars Orbiter Mission (called Mangalyaan meaning Mars craft) should be inserted into Mars orbit. The highly over-rated movie “Gravity” had a larger budget at $100 million than ISRO’s $75 million for its Mars mission.

Ericsson’s headcount in India now exceeds that at HQ in Sweden

June 11, 2014

Ultimately, adding value as close to the customer as possible is not only inevitable but it is also going to be the critical criterion which determines which companies will survive.

Ericsson the Swedish manufacturer of telecommunications equipment has just passed a kind of milestone when its headcount in India has now exceeded the headcount at its headquarters in Sweden. This will be seen negatively in Sweden especially by the unions, but it is this readiness and ability to get close to the market which actually gives me confidence that they are on the right track. Ericsson, I think, have played this balancing act of changing roles at headquarters while growing close to the market rather well. (Which is why I have Ericsson in my portfolio).

Mobiletor: Ericsson which prides itself as a growing provider of communications technology and services, now has more employees in India than it does in its home country of Sweden, according to the company’s Facts & Figures web page. The headcount is 17,991 staff in India and 17,545 employees in Sweden, with about 80 percent of its workforce being male. In total, Ericsson has 111,383 employees from across the world working for it and has its headquarters in Stockholm, Sweden. …..

India is the fastest growing smartphone market on the globe and 4G LTE is still at its nascent stage, with few operators still appearing to be in the mood for testing the waters before diving right in. Going by an Ericsson report, the country’s mobile broadband users will grow in number to touch four times the present figures by the year 2020. This is directly tied to the 80 percent of consumers who still haven’t adopted smartphones and are yet to experience the mobileweb.

Ericsson have a fairly upbeat view of the mobile market in the latest Ericsson Mobility Report and their own prospects:

The number of mobile subscriptions worldwide grew approximately 7 percent year-on-year during Q1 2014. The number of mobile broadband subscriptions grew even faster over this period – at a rate of 35 percent year-on-year, reaching 2.3 billion. The amount of data usage per subscription also continued to grow steadily. Around 65 percent of all mobile phones sold in Q1 2014 were smartphones. Together, these factors have contributed to a 65 percent growth in mobile/cellular data traffic between Q1 2013 and Q1 2014.

By 2019, global mobile broadband subscriptions will exceed the world population.

Total mobile subscriptions are expected to grow from 6.8 billion in Q1 2014 to 9.2 billion by the end of 2019. Global mobile broadband subscriptions are predicted to reach 7.6 billion by 2019 and will gain an increasing share of the total mobile subscriptions over time.

Mobile broadband users in India will grow in numbers to reach four times the present figures by 2020. In 2013, people accessing data on their mobile devices reached 90 million. The smartphone penetration of 10% or 90 million devices will grow to 45% or 520 million mobile gadgets by 2020. The mobile subscriber base is expected to increase from 795 million last year to 1145 million by 2020.