Amateur Radio on the International Space Station- Phase 2 Hardware System
Total Page:16
File Type:pdf, Size:1020Kb
. AMATEUR RADIO ON THE INTERNATIONAL SPACE STATION- PHASE 2 HARDWARE SYSTEM Frank H. Bauer; KA3HD0, Sergej Samburov, RV3DR, Lou McFadin, WSDID; Bob Bruninga, WB4AI'R and Hiroto Watarikawa, JJ 1LYU INTRODUCTION HAM RADIO EOUIPMENT SPECIFICS The International Space Station (ISS) ham radio Ham Station Location system has been on-orbit for over 3 years. Since its first use in November 2000, the first seven The ISS Ham radio equipment will reside in two expedition crews and three Soyuz taxi crews locations inside the ISS and at least one location have utilized the amateur radio station in the outside the ISS. 2-meter (144 MHz) operations Functional Cargo Block (also referred to as the will primarily be conducted inside the FGB or Zarya module) to talk to thousands of Functional Cargo Block (FGB), named Zarya, students in schools, to their families on Earth, using antennas that supported docking of the and to amateur radio operators around the world. FGB with the Russian Service Module. These antennas, designed for use near the 2-meter Early on, the Amateur Radio on the International band, (see figure 1) no longer support docking Space Station (ARISS) international team devised a multi-phased hardware development approach for the ISS ham radio station. Three internal development Phases---Initial Phase 1, Mobile Radio Phase 2 and Permanently Mounted Phase 3 plus an externally mounted system, were proposed and agreed to by the ARISS team. The Phase 1 system hardware development which was started in 1996 has since been delivered to ISS. It is currently operational on 2 meters. The 70 cm system is expected to be FGB 2 Meter Antenna Locations installed and operated later this year. Figure 1 Since 2001, the ARISS international team have and can be used by the ARISS team worked to bring the second generation ham permanently. This is the current location of the system, called Phase 2, to flight qualification 2 meter portion of the Phase 1 ISS ham radio status. At this time, major portions of the Phase station. The FGB radio system represents a 2 hardware system have been delivered to ISS minimal capability that allows the ARISS team and will soon be installed and checked out. to support school group contacts and packet communications on one band, the 2-meter band. This paper intends to provide an overview of the Phase 1 system for background and then The ARKS team's vision of supporting several describe the capabilities of the Phase 2 radio different international users at the same time on system. It will also describe the current plans to separate frequency bands and different modes finalize the Phase 1 and Phase 2 testing in Russia (voice, data, television, etc) requires several and outlines the plans to bring the Phase 2 different antenna systems. The ARISS-Russia hardware system to full operation. team, led by Sergej Samburov, RV3DR, and school students using handheld systems that can be moved throughout the ISS. It will also support communications experimentation that will enable students and radio amateurs to receive telemetry data from ISS. Phase 1 Hardware Overview The ARKS team has developed all the hardware elements for the Phase 1 radio system. These hardware elements have been flown to ISS on ARISS Hardware in Service Module three Shuttle flights. The Phase 1 system Figure 2 supports voice and packet (computer-to- computer radio link) capabilities. Packet radio provided this foundation through the installation has several capabilities including an APRS of four ham radio antenna feedthrough ports on Instant Messaging-type system and a Bulletin the Russian Service Module. With these Board System that allows radio amateurs to store antennas in place, the primary location of the and forward messages and allows the orbiting ham station will reside inside the Russian crew to send e-mail to all hams or to individuals. Service Module (SM) named Zvezda. The ham station will be installed near the SM dining table. The Phase 1 ham radio system was developed See figure 2. Simultaneous multi-band primarily in the US. However, extensive testing operations can be conducted with these two (SM and coordination with the ARISS-Russia team and FGB) station locations. was required since it is installed in the ISS Russian segment. The initial portion of the The ARISS team is also working with the Phase' 1 ISS Ham radio system was launched on- international space agencies to install extemally- board the STS-106 Space Shuttle Atlantis mounted amateur radio equipment on the ISS. mission on September 8, 2000. This system This hardware will enable the crew to consists of two hand-held Ericsson MP-A communicate with Earth-bound radio amateurs transceivers for 2 meters and 70 cm, a power adapter, an adapter module, an antenna w~vewh,F . ISS-HAM Hardware in FGB as of 06/16/01 VEADSFT *.1 SF sCDrClrG system, a packet module, a headset Russan Female assembly, and the required cable RF coiiwinr j 4 assemblies (see figures 3,4 and 5). ; lo :G6 This configuration can be operated in the .-T attended mode for voice communications lril *NE whip and either the attended or T9WSCCIVER VHF iFRlCSSONi MP-A-VHF automatic mode for SIN ow2 packet communications. SXISSS&IN) SiN 1031 Additional ARISS Phase 1 hardware was deployed during two ISS Ham Phase 1 System in the FGB additional Shuttle Ericsson Radio Figure 3 flights to ISS. This Figure 4 hardware included an VHFRJHF flexible additional Packet tape antennas. Module on the STS-105 WA4 includes a Discovery flight on 2.5 meter flexible August 10, 2001 (see tape HF antenna. Figure 6), and additional The antenna cables and modules to systems were support simultaneous 2 developed by the Phase 1 Hardware meter and 70 cm Phase 1 Packet Module U.S., Italian, and Figure 5 operation on the STS- Figure 6 Russian ARISS 108 Endeavour flight on partners. December 5, 2001. Details of the Phase 1 system are described in Each antenna assembly consists of a mounting reference 1. plate, spacer, a black striped handle, a Russian handrail clamp, an orange-colored VHF/UHF (or Antenna Assemblies HF) metal flexible tape antenna with black delrin mounting collar, an L/S band flat spiral antenna In 2002, a set of four antenna systems, with a white delrin radome cover, a diplexer developed by the ARISS team, were deployed (mounted underneath the plate) and during three Russian EVAs. These antennas will interconnecting RF cables. See figure 8. support the Phase 1 and Phase 2 systems in the Service Module. Once checked out, the The specially designed antenna assemblies will antenna permit operations on HF (20 meters, 15 meters systems & 10 meters), VHF (2-meters), UHF (70cm), were and the microwave bands (L and S band) These launched antennas also permit the reception of the Russian on the Glisser EVA video signals (2.0 GHz). This Space dual-use (HadEVA video) capability is the Shuttle F Antenna Systems WA1 -WA4 primary reason the ARISS team received access Endeavour Figure 8 to the four flight on SXISSO96ODHAI lVIU Antnma) SXISSOO407 (EVA CABLE) SXlSSQ0600WA4lHF Antenna: SXISSOO408 (EVA CABLE) antenna December 5, 2001. The two up-looking (zenith) feedthroughs antennas, WA3 and WA4, were deployed by located on the EVA (space walk) in January 2002 and the two outside of the down-looking (Nadir) antennas, WA1 and WA2, Service Module. were deployed by EVA in August 2002. A total of four Antenna installation EVA procedure antenna systems development and training was led by Sergej were developed Samburov from Energia with support from the to get maximum ARISS-USA team. use of the SXISSQS600\\Al(v U Antema) 7700mm sx’ssoo41‘ SXISS99600\112IV,U Anterrno antenna PHASE-2 HARDWARE SYSTEM SNSSOO106 (EVA CABLE) feedthroughs. Antenna Location from __ End of Service Module ‘These were Phase 2 Hardware Overview Figure 7 installed around the periphery-- of The Phase 2 hardware system is expected to the far end of the Service Module. See figure 7. exploit the new antenna systems installed on the Three of the antennas (WA1-WA3) include a Service Module. Two new radio systems will be installed as part of Phase 2. These systems will augment the two Ericsson radio systems already on-board the ISS as part of the Phase 1 system. Combined, the Phase 1 and Phase 2 system will provide more capabilities for the crew and permit simultaneous, multi-mode operations by more than one crew member. The Phase 2 development is a joint Russian, U.S. and Japan activity. Development was led by Russian team member Sergej Samburov, RV3DR. The Russian team was responsible for certifying the hardware for flight and providing the ride on the Progress launch vehicle. The Japanese team provided (donated) the Kenwood radios to the ARISS team and made specific hardware and firmware modifications to the Phase 2 Hardware Housed in radio system to prepare it for flight. The USA Velcro Table team, in conjunction with the Japan and Russian Figure 9 team, developed the Program Memory software that provides a powerful system with a very user-friendly interface for crew. assembly developed by the USA team, a computer and the 70 cm Phase 1 hardware One of the two radios qualified for flight is a system. These will be mounted on a Velcro- Kenwood TM-D700 radio. This radio supports backed table. See figure 9. These radio systems 2 meter (144-146 MHz) and 70 cm (435-438 will be connected to the four Service Module MHz) transmitheceive operation and L-band antenna systems through a Russian developed uplink operation. This radio provides a higher antenna switching system.