The history of small satellites is as old as the history of satellites. In fact, the space age could be said to have begun with the launch of a small satellite, Sputnik-1, in 1957. Until almost the first decade of the 21st century, over 860 micro-satellites, 680 nano-satellites, and 38 pico-satellites were said to have been launched worldwide.1 Though there is no precise statistics available about the exact number of small satellites launched till date, the global interest in small satellites has been growing over the years owing to various factors.
During the initial years of the development of space technologies, the focus was both on developing the satellites and the vehicles capable of launching them. Over a period of time, developments in technology allowed states to position satellites into different orbits. Developments in sensor technology further enhanced the utility of satellite applicability, from ‘a space based observational platform’ to a system as ‘a decision making tool’. Integration of such multipurpose platforms helps governments to take critical decision in various areas, ranging from agricultural planning to disaster management to military operations. Presently, satellites are being increasingly used for meteorology, communication, navigation and other purposes. All these satellite usually have a mass of around two to six tonnes. Other missions like human space missions or development of space stations are required to carry much more mass. Hence, scientific efforts for all these years have normally revolved around designing and developing matching launch vehicles capable of carrying more weight and positioning satellites into different orbits.
With the focus being more on the launching of heavy satellites, the development of launch vehicle technology too has made progression in that direction. Also, states did not face any constraints in regard to their small satellite programmes as it was possible to launch them as 'piggyback' to the heaver satellites.
There are different reasons for growth in small satellite market globally. Since 1950s, development of a rocket launcher for putting satellites into the space has been technologically the most challenging task. Even today, almost six decades after the first satellite was launched, only a handful of states are in a position to launch satellites on their own. All other states are depending on space-faring states (in the recent past, limited private industry players have also developed launch vehicle technology) to launch their satellites.
Today, many smaller states are keen to launch their own satellites (mostly small in type) and are collaborating with space-faring agencies for this purpose. Also, with increase in the capabilities of small satellites owing to various recent technological developments and also understating their increasing strategic utility, space-faring states are found taking renewed interest towards expanding their small satellite development programmes. All this is pushing various space agencies into developing an exclusive new generation of small satellite launch vehicles.
Small satellites serve as low-mass and low-volume platforms that can be sent into orbit in less cost. Satellites could be classified according to their weight, orbit, purpose, etc. As per a standard convention, large satellites are known to have weight above 1000 kg/1tonne, medium satellites fall in the range of 500 kg–1000 kg, and small satellites are known to have maximum of 500 kg weight. Small satellites are further sub-categorised as follows2:
* including fuel
A major advantage with small satellites is that they allow non-spacefaring states, business/scientific establishments, educational institutions, non-governmental organisations and even individuals a low-cost access to space. Small satellites have some limitations owing to power and other sensor-related constraints, though. However, at times, a group of small satellites could undertake functions similar to that of a large satellite in a more cost-effective manner.
The mission life for large satellites is normally more than 10 years (for small satellites less than three years). Hence, most of the functional large satellites are found operating on a decadal old sensor technology. Since the life, cost and launching frequency of the small satellites vary from the large satellites, they could gain from various latest technological innovations and developments. It is obvious from the following table that small satellites are cost-effective investments.
Table 1: Estimated Manufacturing Cost of Satellites Per Kg3
|Mass (kg)||Altitude (km) Orbit Period||Project Lifetime||Total Cost (M US$)||Cost/Mass(k US$/kg)|
|Mini||100 - 500||1000 – 5000
(2 – 3 hrs)
|4 - 7 yrs||10-150||200|
|Micro||10 – 100||500 – 2000
(1.6 - 2 hrs)
|2 - 5 yrs||1-30||400|
|Nano||1 - 10||300 – 800
(1.4 – 1.7 hrs)
|2 - 3 yrs||0.1-10||800|
|Pico||0.1 – 1||200 - 400
(1.4 – 1.5 hrs)
|1 - 2 yrs||0.05-2||1600|
|Femto||< 100 g||200 – 400
(1.4 – 1.5 hrs)
|1 yrs||< 0.05||3200|
Interest in small satellites has leapfrogged during the last few years. As per some estimates4, over the past decade, roughly US$ 2.5 billion has been invested in small satellites and nearly half of that amount has come into play during last one to two years. Also, one of the private operators has announced that they have a plan of putting a constellation of 648 (launching to begin in 2018) small satellites with an estimated cost of US$ 2 billion (not accounted for in the US$ 2.5 billion estimate cited above).
Following graph depicts the actual and projected per year launches of small satellites.5 There is a significant increase expected during next five years in the number of launches.
The above graph is based on information drawn from various sources.
Now, the question is why is there a sudden rush for small satellites? Broadly, following could be the key reasons:
Barring few early years of development in the field of satellites and launch vehicles, small satellites are mostly found being launched as secondary payloads. Also, on occasions, such satellites do get launched from International Space Station (ISS) depending on the nature of specific missions. Aspace-plane too could launch such satellites. However, in all such cases, these satellites get launched only as subset to the main activity. In fact, at times, launch agency is required (read compelled) to launch secondary payload in the form of small satellites as ‘piggyback’ to utilise the full capacity of the launch vehicle.
Over the years, there have been some targeted efforts to develop specific launch vehicles for the small satellites. Currently, in view of the increasing importance of small satellites, various agencies are found making renewed attempts to develop and operationalise small satellite launch systems. Following tables6 provide information about the past, present and proposed small satellite launch systems:
|Vehicle||Origin||Manufacturer||Payload Capacity||First Launch||Last Launch||Launches|
|Mass to LEO (Kg)||Mass to Other Orbits (Kg)|
|Shavit 1/ 2||Israel||IAE||160||1988||2014||9|
Above table indicates that the United States (US) has done more than fifty small satellite launches by using their two specially developed small satellite launch vehicles. Other states like Israel and Russia have undertaken limited launches. In the last three decades, no serious attempts have been made to develop an exclusive small satellite launch system. This indirectly indicates that the global focus during the period was more towards development of big satellites and hence heavy satellite launch systems.
Above table indicates that in the last few years, countries like China and the US have been making investments towards developing small satellite launch systems. The vehicles developed by Iran and North & South Korea should not be strictly viewed from the ‘prism’ of attempt towards developing small satellite launchers. These states have joined the community of space-faring states only during the last few years. Their attempts for many years have been to indigenously develop a rocket which could place a satellite into an orbit. The first step in that direction is to develop a vehicle which could successfully launch minimum weight satellites into the space. Hence, their initial launches have been in the category of small satellites.
Presently, as per the available information, no proposals are in place from Israel and Russia to undertake any major investment in the field of small satellite launches in the near future. Following are the proposals for the US vehicle Orbiter:
Tables 2(a) and 2(b) indicate that China is the only new entrant (state actor) in small satellite launcher field. Few private agencies are also found making investments for developing small satellite launch vehicles. However, the process is facing some challenges owing to which states and private agencies are taking time towards developing such vehicles. At the same time, dependence on regular launch vehicles is also limiting the use of small satellites to their fullest potential. Some such challenges include:
Above points indicate that launching small satellites by using a launcher specifically-designed for the purpose may be desirable, but it is not the best option under the present circumstances. In order to make small satellite launch systems efficient, efforts are being made at two levels: making the existing systems (Vertical Launchers) more competitive, and building upon other launch options like the air launch systems.
Table 3: Air Launch Systems
It is obvious from the above table that the US defence establishment, along with few private agencies, is also keen on developing air launch systems. Such systems are means of launching rockets at an altitude from a conventional horizontal-takeoff aircraft, to carry satellites to the low earth orbit. Such systems are found relevant owing to the reduced mass, thrust and cost of the rocket. Though the Defence Advanced Research Projects Agency (DARPA) of the US has been testing their air launch system since 2012, but is yet to declare it operational.
The table below presents information about few key agencies developing separate systems for the launch of small satellites. They are also using innovative technologies like 3D printing in order to reduce the turnaround time.
Click on table to enlarge
Technological advancement in the field of electronic components, nano-technology, sensor technology and material sciences are leading a revolution in overall satellite building capabilities and launch techniques. Small satellites with their distinct features such as short timelines for development, greatly improved computational capabilities, lesser logistical requirements, and capability to operate as an excellent platform for testing, are making small satellites a popular choice amongst the users.
Small satellites are being increasingly projected as the most in-demand choice for militaries, commercial organisations, educational organisations, etc. However, the increase in demand for small satellites is not supported by the best launch options. Various existing small satellite launch options have huge limitations. It is believed that ‘proliferation’ of small satellites technology is possible only if reliable and cost-effective launch options are made available.
Defence agencies are increasingly looking at small satellites as an important option, essentially for intelligence gathering purposes. Such satellites could also assist in communication and other military-related services. During actual war or in the phase of ‘preparation for the war’, militaries could require positioning of different categories of small satellites as per the battlefield demand. This is only possible if they have the launch-on-demand technology available. Overall, there is a need to develop exclusive small satellite launch systems for various purposes.
Note: All tables in this brief are based on information available in open sources. Several websites have been consulted though only major ones have been cited.