Topic: FBH Developments for Space
FBH developments for space – application under challenging conditions
The communication between satellites and earth is truly demanding with respect to the related technical requirements: Devices need to be particularly reliable and robust so that they can survive a rocket launch and work properly under the harsh conditions in space (radiation, thermal variations). FBH laser benches, for example, still work flawlessly on board of several communication satellites since 2008. The institute has long-term and comprehensive experience in this field, working in projects with the European Space Agency ESA and the German Aerospace Center DLR. A variety of R&D projects deal with spaceborne technologies, including optical communications, quantum optical metrology, beam steering technologies and energy-efficient electronics for satellites. At the same time, FBH components developed for space are technology drivers for a multitude of terrestrial applications.
Optical communications – from earth to space
Driven by the ever-increasing data traffic, optical communication technology is going to conquer space. Therefore, ESA introduced the European Data Relay System (EDRS), a space data highway supporting real-time data links for earth observation satellites, scientific missions or high flying aircrafts with global, ubiquitous coverage. Tesat-Spacecom supplies the required laser communication terminals that enable 1,000 times higher frequency and thus much higher transmission rates than conventional radio-based communication. Moreover, laser beams can be directed at low divergence over long distances, which allows for low-error detection and protection of sensitive data. Ferdinand-Braun-Institut contributes the required sophisticated semiconductor pump sources offering highest robustness, reliability, and low-noise properties.
Laser systems for spaceborne quantum optical metrology
Since 2008, FBH has been developing and delivering miniaturized laser modules for experiments under micro-gravity conditions – in a drop tower as well as on board sounding rockets. Within a consortium of German research labs, FBH has successfully flown several laser modules during three distinct sounding rocket missions – among them MAIUS, where the first-ever Bose-Einstein condensate in space was created.
During this time span, FBH has been constantly improving its diode laser and hybrid micro-integration technology, thus advancing electro-optical performance and achieving better resilience of the laser modules to harsh environments. FBH’s micro-integrated laser modules for space applications are fully packaged, fiber-coupled, and deliver high output power together with narrow linewidth. They have been designed for very high-performance precision experiments and coherent communications on satellites – including upcoming missions as part of an iodine-based frequency reference on a sounding rocket and for deployment into a cold atom laboratory on the International Space Station (ISS).
Further information regarding FBH's activities on micro-integrated laser modules for space applications.
Article on quantum technologies including FBH's activities (Jan. 2018, Laser Focus World)
Energy-efficient electronics for satellites
Power consumption and dissipated power are critical issues when operating solid-state power amplifiers (SSPAs) in space. Envelope tracking (ET) is a well-known efficiency enhancement technique for SSPAs modulating the supply voltage of the RF power amplifier (PA) in accordance to the instantaneous signal envelope. One of FBH’s ESA-funded projects deals with a reverse-buck topology targeting satellite applications in the L-band. The challenge behind this topology is that it requires a floating-ground RF PA. Prototypes achieve already promising results. For future wideband systems in the 18…20 GHz range, FBH researchers investigate an alternative ET solution with excellent efficiency, which is discrete supply modulation, also known as class G.
FBH has also been working on decentralized PAs and receivers based on GaN which are required for beam steering and phased-array radar systems. This includes a European satellite project aiming at beam steering techniques for 30 GHz uplink and 20 GHz downlink communication. In addition, FBH´s normally-off power transistors are currently undergoing comprehensive stress tests to be implemented in future spaceborne electronic power conditioners.
Data highway in space - ultrafast optical communication at highest data rates
For more than 20 years, the Ferdinand-Braun-Institut has been closely cooperating with Tesat-Spacecom, the world’s leading company in the field of optical satellite communication. Tesat supplies laser communication terminals (LCT) on behalf of the German Aerospace Center (DLR) as core components of the European Data Relay System (EDRS). This space data highway uses optical links to transfer information with highest data rates between low-orbiting and geostationary satellites. The latest LCT generation enables a data transmission rate in space of several Gbit/s over long distances up to 80,000 km. Based on the principle of coherent bidirectional transmission, the LCT is equipped with two frequency-stabilized Nd:YAG solid-state lasers, namely a transmitter and a local oscillator acting as demodulator to detect the received messages. These Nd:YAG lasers are pumped with FBH’s semiconductor laser modules that offer high frequency stability, low intensity noise, and a long operating life under continuous temperature cycling and extraterrestrial irradiation.
FBH’s laser diode benches – a power boost for laser communication
FBH has developed and qualified its laser diode benches (LDB) according to the standards of the European Space Agency (ESA) for space applications. The devices are designed to meet the extreme requirements of the LCT. The wavelength of the laser beam is stabilized to the pump transition band of the Nd:YAG (808 nm) while preventing the laser intensity to fluctuate in time, thus ensuring stable LCT performance. Furthermore, the diode laser must continuously operate over the mission’s lifetime of 15 years with proven reliability (99.9% on system level). This goal is achieved by a dedicated design keeping the power density small and including non-operating spare parts. Recent research efforts at FBH focus on novel concepts for on-chip integration of a sophisticated wavelength stabilizer, yielding both low noise and high reliability.
Reliable data transmission in space
Coherent transmission of data using LDBs from FBH was first demonstrated in 2008 between the satellites TerraSAR-X and NFIRE with an unprecedented rate of up to 5.6 Gbit/s over 5,000 km and from satellite to earth. Subsequently, the institute’s devices were used in all further communication links established within EDRS. The focus was on low earth orbit (LEO) communication, but has been successfully tested also for the geostationary orbit (GEO) with Alphasat I-XL. In 2016, the first satellite of EDRS-A was launched into GEO, receiving images from earth through LCT transmission collected by Sentinel 1A on LEO to be then transmitted to the ground station without significant time delay. By 2021, three EDRS satellites placed in GEO shall be continuously accessible from almost every LEO position. This way, an optical network consisting of laser beams through space and relay satellites as switching nodes will be realized, thus opening a new dimension for the future of optical communications.
Further information regarding FBH's contribution to EDRS.
Laser systems for spaceborne quantum optical metrology
FBH develops particularly compact and stable laser systems for harsh environments. Since 2008, the institute closely cooperates with Humboldt-Universität zu Berlin within its research area Integrated Quantum Technology (former Joint Lab Laser Metrology), developing the laser systems required for QUANTUS (quantum gases in microgravity). The DLR-funded project investigates fundamental laws of physics with cold atoms as microscopic test masses under microgravity conditions performed in a drop tower and on board sounding rockets.
Meanwhile, laser systems developed by the Joint Lab Laser Metrology have been successfully applied in three sounding rocket missions, thus demonstrating their outstanding performance and reliability. In January 2017, as part of the MAIUS mission, a Bose–Einstein condensate (BEC) was created for the first time in space. In April 2015 and in January 2016, technological components of the MAIUS mission were successfully tested in the experiments FOKUS and KALEXUS.
Such experiments are innovation drivers for a wide range of applications, from GPS-free navigation to spaceborne geodesy. Moreover, with the advent of the "second quantum revolution", it is highly attractive to bring such technologies to market. The Joint Lab Laser Metrology has already taken up the challenge of developing laser systems for future portable quantum-technology-based devices.
Flexible technology platform for long-term space missions
The laser system of MAIUS was developed to perform laser cooling and atomic interferometry with ultra-cold rubidium atoms on a sounding rocket platform. It is based on a master oscillator power amplifier (MOPA) architecture with a DFB laser (MO) delivering narrow-linewidth (~ 1 MHz) laser light with low optical power and a tapered amplifier (PA) that ramps up the MO power up to some watts without degradation of linewidth. The MOPA is implemented on a ceramic substrate via hybrid micro-integration of laser chips, micro-optics, and discrete electronics.
The Joint Lab scientists have used their experience gained from the experiments with the MAIUS laser modules and applied this when developing the MiLas family of lasers. As a result, a laser technology for cold atom sensors on satellites is now available. Features include sealed housings, plugged electrical contacts, fiber-coupled inputs and outputs, and integrated thermal management. The concept of ECDL (extended cavity diode laser)-MOPA has been implemented for the first time within a single laser unit, achieving linewidths < 100 kHz with output powers ex single-mode, polarization-maintaining fiber > 500 mW.
The first MiLas ECDL-MOPA emitting at a wavelength of 1064 nm has already been delivered and will be flown on a sounding rocket in the JOKARUS experiment, as part of an iodine-based frequency reference. The MAIUS-II experiment, with atom interferometry on species of rubidium and potassium on board a sounding rocket also implements ECDL-MOPA's emitting at 767 nm, 780 nm and 1064 nm. The next step is planned on the International Space Station (ISS), again with atom interferometry experiments. However, the MiLas laser modules also meet the requirements for a variety of alternative applications in space, for example coherent optical communications as well as for precision distance measurements. They are also designed to expand even deeper into space, be it in the context of "big-space" with high-performance spacecrafts or in the emerging context of "micro-space" on, for example, the CubeSat platform.
Advanced micro-integration techniques
FBH has comprehensive experience in merging inherently energy-efficient diode lasers with advanced micro-integration techniques optimized to fit the respective application – including operation in harsh environments like space. High performance within a minimal footprint requires high integration density. For the optics, for instance, this implies using lenses with very small focal lengths, usually from a few 100 µm to a few mm. Efficient beam shaping, beam steering, and coupling into waveguides with typical dimensions of some µm can then only be achieved by very tight positional tolerances on the optics, in some cases well below 100 nm.
For deployment in space, it is required that integrated optics keep their precise alignment after facing vibrations, shocks or rapid thermal variations. Stability of components and processes is therefore comprehensively tested and validated during all development stages. One of the most sensitive functionalities in this context is on-board single-mode, polarization-maintaining fiber coupling with high efficiency (> 70% coupling efficiency at power levels > 600 mW). The concept relies on very fine control of the angular alignment (< 0.001°) of the divergent output beam from a diode laser or an amplifier, first collimated via micro-optics and subsequently coupled into a fiber coupler via micro mirrors.
The on-board fiber-coupling concept was tested sequentially against random vibrations at 8 gRMS and 30 gRMS, shocks of up to 1500 g, and 100 thermal cycles between -55°C and +70°C. Within measurement uncertainty, no loss of fiber-coupling efficiency was observed. This concept has been successfully implemented in FBH’s micro-integrated laser modules for space applications.
Further information regarding FBH's hybrid microintegration technologies.
Energy-efficient electronics for satellites
Energy consumption and dissipated power are critical issues when operating microwave and mm-wave solid-state power amplifiers (SSPAs) in space, because the available DC power is limited and heat removal is hindered. However, conventional power amplifiers achieve the highest efficiency in the saturation region, where linearity is reduced. FBH is addressing this contradictory problem with two alternative solutions. In addition, FBH is working on GaN-based solutions for phased array systems for satellite communications at Ku-Band.
Envelope tracking based on a reverse buck converter
A well-proven efficiency enhancement technique is envelope tracking (ET), which modulates the supply voltage of the RF power amplifier (PA) in accordance to the instantaneous signal envelope. In a project financed by the European Space Agency (ESA) FBH develops such a system with the envelope amplifier (EA) in a reverse buck converter topology. The gate-source control of the final-stage transistor in the EA is operating with the source grounded. Thus, the load, i.e., the RF PA, is operating with a floating ground. Unlike in conventional buck converters, there is no need for an isolated gate driver in the EA. As a consequence, it features lower switching propagation delay enabling improved closed-loop control bandwidth. The proof-of-concept demonstrator operates at 1620 MHz and 40 V supply and shows 39% overall power-added efficiency (PAE) at an average output power of 14.6 W for an 8 MHz modulated signal with 8.6 dB peak-to-average power ratio (PAPR). The reverse buck converter switches at 45 MHz with a PAE of 80 - 91% for 16 - 40 V supply voltages. For the first time, a reverse buck topology system enabling GaN switching operation referred to ground has been shown in dynamic operation.
Advanced K-band power amplifiers with discrete supply modulation
Another promising concept for space applications in the K-band evaluated at FBH is the class-G topology or discrete supply modulation. Here, the supply voltage is modified in discrete steps according to the instantaneous signal envelope. A first quasi-static evaluation, applying this concept to the 0.15 µm FBH GaN-HEMT technology, shows a possible efficiency improvement of 13%-points using a 2-level supply modulation at 20 GHz, operating with a 9 dB PAPR signal. Furthermore, the dissipated power can be reduced to 1/3 compared to fixed supply-voltage operation. This enables alternative architectures with reduced cooling effort, smaller footprint, and less weight. At present, the first integrated MMIC designs are being fabricated and novel approaches for digital isolation are being evaluated.
GaN technology for beam steering antennas and phased array systems
Realizing very efficient microwave power amplifiers enables powerful decentralized communication and radar systems where the broadcasted power is superimposed in the far-field of a multitude of antennas grouped in a linear or 2-dimensional array. Such arrangements are suitable for beam steering antenna and phased array systems. Among others, this technique is used in low-altitude earth orbiting satellites to track different ground stations and users electronically without any movable mechanical antenna parts. In a European project, FBH has developed the GaN chip technology for such a spaceborne system. Uplink power amplifiers at Ku-band delivering 13 W output power at 18 GHz with a PAE of 46%, and low-noise receivers at Ka-band (30 GHz) with a noise figure of 2.7 dB have been demonstrated and delivered to partners for antenna array integration.