Development of the ISS Russian Segment in 2010

Development of the ISS Russian Segment in 2010 – 2020

A. Markov, A. Kaleri May 2011 © S.P. Korolev Rocket and Space Corporation Energia, 2011 ISS Russian Segment in 2009

NumberNumber of of Modules Modules 33 Mass,Mass, т т 5454 PSSPSS Capacity, Capacity, kW kWup up to to66 3 PressurizedPressurized Volume, Volume, m m3 170170 FGB Zarya (1998, Proton Launcher) USOS

Service Module Zvezda (2000, Proton Launcher)

ISS021E030672

Docking Compartment 1 Pirs (2001, Soyuz Launcher) ISS Russian Segment in 2010

MRM1 «Rassvet» docked to the ISS RS Space Shuttle Atlantis is on the background

NumberNumber of of Modules Modules 55 Mass,Mass, т т 6767 PSSPSS Capacity, Capacity, kW kWup up to to66 3 PressurizedPressurized Volume, Volume, m m3 200,5200,5 ISS023Е047527

РЕЗЕРВ

ISS Russian Segment in 2010 ISS Russian Segment, Second Phase (2015)

Mini Research Module 2 Poisk

FGB Zarya Service Module Zvezda

The ISS Russian Segment Mini Research Module 1 Rassvet

Multipurpose Number of Modules 8 Laboratory Module Number of Modules 8 Mass,Mass, т т 132132 PSSPSS Capacity, Capacity, kW kW 2020 3 PressurizedPressurized Volume, Volume, m m3 470470

Scientific-Power Module 1 (2014, Proton Launcher)

Scientific-Power Module 2 Node Module (2015, Proton Launcher) (2013, Soyuz Launcher) International Space Station after completion of the Russian Segment construction

Key Features Number of Modules 16 Total Mass, т 374 PSS Capacity (average daily), kW 110 Total Pressurized Volume, m3 839 Research Facilities on the ISS Russian Segment

Principles of Payloads Integration

Payloads accommodation on the ISS RS modules is implemented on the basis of the exchangeable payloads method with use of the universal workstations (UW)

In-flight installation and accommodation of a payload on the module’s UWs is carried out

UWs are equipped with mechanical, power, information, and other interfaces to support a payload functioning

Payloads exchange is implemented on the basis of rotation principle in compliance with execution of the research program or the equipment failure Mini Research Module 2 «Poisk»

Mini Research Module 2 (MRM2) – the forth element of the ISS RS, meant for implementation of service functions (similarly DC1) , as well as investigations in accordance with scientific program

The module has been launched on November 10, 2009, is mated to the ISS – since November 12, 2009

Is used for the research program implementation since January 2010

ISS021E030653 Mini Research Module 2 «Poisk»

LAUNCH MASS, KG 7290

MASS OF MODULE, KG 4000

PRESSURIZED VOLUME, М3 12,5

CARGOES INSIDE, КГ 1000

WORKSTATIONS 2

Task - Increasing of the ISS RS resources Docking port Airlock Pressurized volume New workstations for research hardware Research Facilities on MRM2

External workstation for payloads accommodation URM-D UW utilization on MRM2 will allow increasing number of sites/adapters for the external payloads accommodation from one to three

Platform equipped with Base adapters

Holding plates Universal Workstation URM-D for external payloads accommodation Research Facilities on MRM2

An example of the experiments accommodation on SM using the same type of URM-D

ROKVISS, «Impuls», and EXPOSE-R Experiments ROKVISS Experiment installed on the installed on the URM-D URM-D (photo) Research Facilities on MRM2

Internal Workstations

Workstations near the module’s windows PK-3+ Workstation (allocated volume - 0.18 m3) Mini Research Module 1 «Rassvet»

Mini Research Module 1 (MRM1) – the fifth element of the ISS RS. Its main purpose after putting into operation is implementation of scientific experiments in accordance with the research program

The module after preparation for flight in the USA was delivered to the ISS aboard Atlantis orbiter (STS-132 mission) and integrated to the ISS RS on May 18, 2010 Mini Research Module 1 «Rassvet»

MRM1 integration with the ISS Russian segment Mini Research Module 1 «Rassvet»

LAUNCH MASS, KG 7900

PRESSURIZED VOLUME, М3 18

CARGOES STORAGE, М3 5

CARGOES INSIDE, KG 1400

CARGOES OUTSIDE, KG 1800

WORKSTATIONS 8

Tasks: Increasing of the ISS RS resources New workstations for scientific equipment Docking port Pressurized volumes Scientific research implementation MRM1 Payloads Complex

Features of the MRM1 Utilization

In the module’s pressurized compartment 8 UWs are established

─ 4 UWs will be equipped with the onboard support facilities: Glovebox (Glovebox-C) Universal biotechnological incubator for lower temperature (TBU-N) Universal biotechnological incubator for higher temperature (TBU-V) Vibroprotective platform (VZP-U)

─ 4 UW will be equipped with mechanical adapters for payloads installation: roll-out racks/shelves

The Module inside: delivered cargoes unloading, ISS-23, Russian cosmonaut Alexander Skvortsov Research Facilities on MRM1

Onboard support facilities and mechanical adapters’ accommodation

Starboard Starboard AllocatedAllocated volume volume for for the the HW HW accommodation: accommodation: 3 - payloads (experiments) 0.68 m3 ; - payloads (experiments) 0.68 m ;3 -- support support facilities facilities 1.36 1.36 m m3

WorkstationsWorkstations equipped equipped withwith roll-out roll-out racks/ racks/ Workstation of shelvesshelves (behind (behind the the Workstation of Workstation of Workstation of Glovebox (behind the interiorinterior panels panels TBU-V (behind the Glovebox (behind the TBU-V (behind the interior panels NoNo 401, 401, 402) 402) interior panel interior panels interior panel Workstation of VZP-U (behind the No 405, 406) NoNo 403) 403) Workstation of VZP-U (behind the No 405, 406) interiorinterior panel panel No No 404) 404) Research Facilities on MRM1

Onboard support facilities and mechanical adapters accommodation

AllocatedAllocated volume volume for for the the HW HW Port side accommodation: Port side accommodation: 3 - payloads (experiments) 0.68 m3 ; - payloads (experiments) 0.68 m ;3 -- support support facilities facilities 0.34 0.34 m m3

WorkstationsWorkstations equipped equipped with with roll-out roll-out racks/ racks/ shelves shelves (behind(behind the the interior interior panels panels No No 204, 204, 206) 206) WorkstationWorkstation of of TBU-N TBU-N (behind (behind the the interior interior panelpanel No No 205) 205) Research Facilities on MRM1

Glovebox-C

Meant for operations with sterile, dangerous or free-flowing substances with 99,9% purification rate of the working chamber air

Provides: means of locking, cleaning, and sterilization; volume – 0.25 m3 ; number of service ports – 5.

Glovebox-CGlovebox-C HardwareHardware

Roll-outRoll-out Shelf Shelf Research Facilities on MRM1

Universal biotechnological incubator for higher temperature (TBU-V)

VZP-UVZP-U Oscillator Oscillator

TBU-VTBU-V

Provides: required temperature conditions to support operations with bioobjects; net volume 16 L; temperature control range +(2…37 )оС. Research Facilities on MRM1

Multipurpose vibroprotective platform VZP-U

VZP-UVZP-U platformplatform

Provides: protection against onboard vibrations with vibroinsulation rate by 20 dB in frequency range ∆f = 0.4-250 Hz; mass of mountable hardware – up to 100 kg

«Reka»«Reka» hardwarehardware (will(will be be installed on Power and control installed on Power and control VZP-UVZP-U in in 2011) 2011) systemsystem of of «Reka» «Reka» experimentexperiment Research Facilities on MRM1

Mechanical adapters

Frame-ArchFrame-Arch ProvidesProvides capability capability to to installinstall up up to to 4 4 shelvesshelves- modulesmodules on on 10 10 levels levels

Shelf-Module Shelf-Module Moves forward up to 400 Moves forward up to 400 mm, provides a payload mm, provides a payload fastening fastening ISS Russian Segment, First Phase (2012)

Mini Research Module 2 Poisk FGB Zarya

Service Module Zvezda

Mini Research Module 1 Progress-M Rassvet Cargo Vehicle (2010, Space Shuttle)

NumberNumber of of Modules Modules 55 Mass,Mass, т т 8787 Multipurpose Laboratory PSSPSS Capacity, Capacity, kW kWup up to to1616 Module (from(from USOS) USOS) (2012, Proton Launcher) Pressurized Volume, m3 258 Soyuz TMA Spacecraft Pressurized Volume, m3 258 Исп.: А.Н.Щукин, отдел 101, т. 3-06-89, 2010 г. Multipurpose Laboratory Module (MLM)

Key Specifications Purpose ● Expansion of Research program on the ISS RS with use: Launch mass, kg...... 20 700 - universal workstations inside and outside the module; Volume of pressurized compartment, m3 . . . . . 70 - vibroprotective platforms; Volume for cargoes storage, m3 ...... 8 -glovebox; - incubators. 3 Volume for research facilities, m ...... 8 ● Development and application of robotic systems: Window Ø426 mm ...... 1 - ERA robotic arm; - automated lock-chamber. Power for research equipment, kW...... ≤2.5 ● Providing capabilities for further development of ISS RS Number of workstations , outside/inside . . . . 13/16 MLM External UW for the Research Facilities Accommodation

I Plane view

UW-H1

UW-H2

UW-H10

UW-H7 UW-H9 Lock-Chamber MLM External UW for the Research Facilities Accommodation

III Plane view

PUW (Portable UW) UW-H5

ERA (position for storage)

UW-H6

UW-H3

Lock-Chamber UW-H8

UW-H11 MLM Lock-Chamber (LC) Исп.: А.Н.Щукин, отдел 101, т. 3-06-89, 2010 г.

Key Specifications Purpose Mass, kg ...... ≤1050 ●Extraction of payloads from the MLM pressurized Average daily power consumption, kW ...... 0.08 adapter for their installation outside the station; Max power consumption (including payload) , kW 1.5 ●Payloads acquisition from ERA robotic arm and their Volume, m3 ...... 2.1 relocation into the inner volume of LC and than – into Maximum maintainable payload mass, kg. . . . . 150 the pressurized adapter of MLM; Number of vacuumization cycles ...... >200 ●Carrying out of scientific experiments in the inner 2 Allowable internal pressure, kg/сm ...... 1.3 space of LC; Residual pressure at evacuation, mm Hg ...... 10-4 ●Carrying out of scientific experiments outside LC with Orbital service life, years...... 15 use of its sliding worktable and/or a specialized Way of delivery on the ISS...... as part of workplace. MRM1 Multipurpose Laboratory Module (MLM)

MLM Maintenance of LC with use of ERA robotic arm

Payload

LC ERA Implementation of Russian research program in 2011 on the ISS RS modules (SM, DC1, MRM1, MRM2) and on Progress cargo spacecraft

60 experiments in total MRM2 Sessions of 4 experiments: Identification, Biodegradation, Matroshka, Izgib are Inside of pressurized carried out on all modules of the ISS RS compartment 2 experiments Plasma Crystal, Coulomb Crystal

SM+DC1 50 experiments On the external surface 9 experiments BTN-Neutron, Vsplesk, Biorisk, Vynoslivost’, SLS, Molniya-Gamma, Obstanovka, Radioskaf, SVTch- Radiometriya Inside of pressurized MRM1 compartments 41 experiments Inside of pressurized compartment Progress 2 experiments 2 experiments Aseptic, Membrane Radar-Progress, Microsputnik Service Module of the ISS RS

First element of the ISS Russian Segment

Launched on - 12.07.2000

Beginning of the Research program implementation - 02.11.2000

Since the module’s initial habitation (within 2000-2010) on SM were carried out 309 experiments, including 92 ones implemented within the scope of Russian Research Program Research Facilities on SM

Expose-R Facility (Expose Experiment) REU Monoblock Antenna Unite (ROKVISS Experiment) GTS Experiment

Multipurpose Workstation (URM-D) Port Side

Pulse-plasma Injector (Impulse Experiment)

Multipurpose Spectrometer Workstation (Vsplesk Experiment) (URM-D) Starboard

Research Facilities accommodation on the external surface of SM (2010) RF Receiver-Transmitter with Antenna (CUP) (Kontur Experiment)

- Installed in 2010 Research Facilities on SM

Expose-R Facility (Expose Experiment) Antenna Unite (GTS Experiment) Microwave Radiometer РК-21-8 (SVTch-Radiometriya Experiment)

Plasma-wave Hardware Complex (Obstanovka Experiment) Laser Communication System Terminal Forecasting Hardware (SLS Experiment) Complex (Seismoprognoz Experiment) Photon-Gamma Instrument (Molniya-Gamma Experiment)

Spectrometer (Vsplesk Experiment)

Plasma-wave Hardware Complex (Obstanovka Experiment) High-rate Data Downlinking System (for MKS-Napor Experiment) Research Facilities accommodation on the external surface of SM (2011) Research Facilities on SM

All-sky Monitor Instrument Biaxial Payload Pointing Platform (All-sky Monitor equipped with a Experiment) Hyperspectrometer (MKS-Napor Experiment)

Photon-Gamma Instrument (Molniya-Gamma Experiment) Microwave Radiometer РК-21-8 (SVTch-Radiometriya Experiment)

Plasma-wave Hardware Complex Plasma-wave (Obstanovka Experiment) Hardware Complex (Obstanovka Experiment) Forecasting Hardware Complex (Seismoprognoz Experiment)

Research Facilities High-rate Data Downlinking System Multi-layer Scintillation (as a part of MKS-Napor Experiment) accommodation on the Spectrometer (Alpha-electron Experiment) external surface of SM (2012) Research Facilities on SM

EarthEarth surface surface mapping mapping in in visible visible and and infraredinfrared bands bands Installation of a Biaxial Pointing Platform equipped with a Hyperspectrometer URM-D (MKS-Napor Experiment) on URM-D (Starboard)

Side-mounted Workstation

Biaxial Pointing Platform

PointingPointing platform: platform: •mass•mass – – 47 47 kg kg •positioning•positioning error error – – 10 10 ‘ ‘ Hyperspectrometer:Hyperspectrometer: Hyperspectrometer •Mass•Mass – – 30.5 30.5 kg kg 2012 • •numbernumber of of spectral spectral channels channels – – 70 70 2012 • •spatialspatial resolution resolution – – 30 30 m m Biaxial Pointing Platforms on the ISS RS

Biaxial Pointing Platform “Lutch” (“Beam”)

KeyKey SpecificationsSpecifications

--PayloadPayload mass,mass, kgkg ≤≤6565 -- Payload’s Payload’s momentmoment ofof inertia,inertia, kg*mkg*m22 ≤≤2525 -- Slewing Slewing angle,angle, deg.deg. ++175175 -- Angular Angular velocityvelocity,, ang.ang. min./smin./s :: minmin 1.01.0 maxmax 3.03.0 -- Angular Angular positioningpositioning error,error, ang.ang. min.min. 1010 -- Specified Specified life,life, hrshrs 15001500 Developer: VNIITRANSMash State Enterprise

Biaxial Rotating Platform (DPP)

DPPDPP SpecificSpecific FeaturesFeatures

--PayloadPayload massmass increasincreaseded upup toto 100100 kg;kg; --Platform’sPlatform’s specifiedspecified lifelife hashas beenbeen increasedincreased upup toto 2500025000 hrs hrs thanksthanks toto gearlessgearless drivesdrives application application

Developer: TsNIIRTK State Enterprise Components of Plasma-wave Hardware Complex (Obstanovka Experiment)

CWD1 BSTM

CWD2

DP CORES

BCS RFA Antennas

№ Component Name Code Developer 1 Combined Wave Sensor CWD Ukraine, Russia 2 Fluxgate Magnetometer with Analog Output DFM1 Russia 3 Fluxgate Magnetometer with Digital Output DFM2 Ukraine 4Langmuir Probe LP Bulgaria 5Potential Sensor DP Bulgaria 6 Correlation Electron Spectrograph CORES England DFM 7 Radio Frequency Analyzer RFA Poland, Sweden Probe 8 Analyzer of Low-frequency Radiation SAS3 Hungary 9 Data Analysis and Control Unite DACU Hungary 10 Telemetry Information Storage Block BSTM Hungary 11 Temperature Control Automatic System ASOTR Russia LP 12 Beams for Sensors Carrying-over BSC Russia On-board Terminal of Laser Communication System (BTLS)

BTLS Configuration RSE-LCS

External Block – BTLS-N Internal Block – BTLS-V ISS RS Support Laptop – RSE-LCS

BTLS-V Developer: NPK SPP Corp.

Key Specifications BTLS-N

Hardware mass, kg - 98.5 Data transmission rate, Mb/s - 75 Data receiving rate, Mb/s - 2 Communication session duration, min - up to 5 Transinformation content per session, Gb - up to 3

Terrestrial Terminal of Laser Communication System (NTLS) Progress Cargo Space Transportation Vehicle

Progress M, M1, M-M Key Specifications

Launch mass, kg 7290-7440 Cargo mass, kg 2300-2550 including «dry» cargo 1200-1700 Volume of cargo compartment, m3 7 Free flight duration, days up to 30 Duration of mated flight with ISS, days up to 180 Use of Progress-M Vehicle in Goal-Oriented Programs

Chibis microsatellite Launching of satellites and In-flight development tests of a special (Institute of Space Research, recoverable ballistic capsules purpose hardware RAS)

Delivery in orbit of large-size blocks of HW mounted in the vehicle’s structure Chibis Microsatellite

Developer of the microsatellite – Institute of Space Research of Russian Academy of Sciences

Purpose – investigation of new physical mechanisms of electrical discharges in the Earth atmosphere

1) Mass – 40 kg, including scientific equipment mass – 12.5 kg 2) Downlinking system capacity – 1.2 Mb/s

Progress-M cargo space vehicle is used for delivery of microsatellite robotically onto the orbit with an altitude about 500 km In-flight Development Tests of Large-size Structures Using Progress-M Vehicle

Automatic unfolding of antennas and other special purpose large-size structures

Automatic unfolding of large-size film reflectors

Installation of large-size structures Development of the ISS Russian Segment in 2010 – 2020

A. Markov, A. Kaleri May 2011 © S.P. Korolev Rocket and Space Corporation Energia, 2011 Development of the ISS Russian Segment in 2010 – 2020

A. Markov, A. Kaleri May 2011 © S.P. Korolev Rocket and Space Corporation Energia, 2011 Additional Slides • In case you have questions in payload integration on the Russian segment of the ISS please feel free to contact with Dr. Igor Sorokin by e-mail: [email protected]