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Maintenance Strategy and Its Importance in Rocket Launching System-An Indian Prospective
ISSN(Online) : 2319-8753 ISSN (Print) : 2347-6710 International Journal of Innovative Research in Science, Engineering and Technology (An ISO 3297: 2007 Certified Organization) Vol. 5, Issue 5, May 2016 Maintenance Strategy and its Importance in Rocket Launching System-An Indian Prospective N Gayathri1, Amit Suhane2 M. Tech Research Scholar, Mechanical Engineering, M.A.N.I.T, Bhopal, M.P. India Assistant Professor, Mechanical Engineering, M.A.N.I.T, Bhopal, M.P. India ABSTRACT: The present paper mainly describes the maintenance strategies followed at rocket launching system in India. A Launch pad is an above-ground platform from which a rocket or space vehicle is vertically launched. The potential for advanced rocket launch vehicles to meet the challenging , operational, and performance demands of space transportation in the early 21st century is examined. Space transportation requirements from recent studies underscoring the need for growth in capacity of an increasing diversity of space activities and the need for significant reductions in operational are reviewed. Maintenance strategies concepts based on moderate levels of evolutionary advanced technology are described. The vehicles provide a broad range of attractive concept alternatives with the potential to meet demanding operational and maintenance goals and the flexibility to satisfy a variety of vehicle architecture, mission, vehicle concept, and technology options. KEY WORDS: Preventive Maintenance, Rocket Launch Pad. I. INTRODUCTION A. ROCKET LAUNCH PAD A Launch pad is associate degree above-ground platform from that a rocket ballistic capsule is vertically launched. A launch advanced may be a facility which incorporates, and provides needed support for, one or a lot of launch pads. -
Overview of Sensors for Applications
OVERVIEW OF SENSORS FOR APPLICATIONS Deepak Putrevu Head, MTDD/AMHTDG EM SPECTRUM Visible 0.4-0.7μm Near infrared (NIR) 0.7-1.5μm Optical Infrared Shortwave infrared (SWIR) 1.5-3.0μm Mid-wave infrared (MWIR) 3.0-8.0μm (OIR) Region Longwave IR(LWIR)/Thermal IR(TIR) 8.0-15μm Far infrared (FIR) Beyond15μm Gamma Rays X Rays UV Visible NIR SWIR Thermal IR Microwave P-band: ~0.25 – 1 GHz Microwave Region L-band: 1 -2 GHz S-band: 2-4 GHz •Sensors are 24x365 C-band: 4-8 GHz •Signal data characteristics X-band: 8-12 GHz unique to the microwave region of the EM spectrum Ku-band: 12-18 GHz K-band: 18-26 GHz •Response is primarily governed by geometric Ka-band: 26-40 GHz structures and hence V-band: 40 - 75 GHz complementary to optical W-band: 75-110 GHz imaging mm-wave: 110 – 300GHz Basic Interactions between Electromagnetic Energy and the Earth’s Surface Incident Power reflected, ρP Reflectivity: The fractional part of the radiation, P incident radiation that is reflected by the surface. Power absorbed, αP Absorptivity: the fractional part of the = Power emitted, εP incident radiation that is absorbed by the surface. Power transmitted, τP Emissivity: The ratio of the observed flux emitted by a body or surface to that of a P= Pr + Pt + Pa blackbody under the same condition. 푃 푃 푃 푟 + 푡 + 푎 = 1 푃 푃 푃 Transmissivity: The fractional part of the ρ + τ + α =1 radiation transmitted through the medium. At thermal equilibrium, absorption and emission are the same. -
Indian Payload Capabilities for Space Missions
INDIAN PAYLOAD CAPABILITIES FOR 13, Bangalore - SPACE MISSIONS July 11 A.S. Kiran Kumar Director Space Applications Centre International ASTROD Symposium, Ahmedabad th 5 Application-specific EO payloads IMS-1(2008) RISAT-1 (2012) MX/ HySI-T C-band SAR CARTOSAT-2/2A/2B RESOURCESAT-2 (2011) (2007/2009/2010) LISS 3/ LISS 4/AWiFS PAN RESOURCESAT-1 (2003) LISS 3/ LISS 4 AWiFS CARTOSAT-1 (2005) (Operational) STEREOPAN Megha-Tropiques (2011) TES(2001) MADRAS/SAPHIR/ScARaB/ Step& Stare ROSA PAN OCEANSAT-2 (2009) OCM/ SCAT/ROSA YOUTHSAT(2011) LiV HySI/RaBIT INSAT-3A (2003) KALPANA-1 (2002) VHRR, CCD VHRR Application-specific EO payloads GISAT MXVNIR/SWIR/TIR/HySI RISAT-3 RESOURCESAT-3A/3B/3C L-band SAR CARTOSAT-3 RESOURCESAT-2A LISS 3/LISS 4/AWiFS PAN LISS3/LISS4/AWiFS RESOURCESAT-3 LISS 3/LISS 4/ CARTOSAT-2C/2D AWiFS (Planned) PAN RISAT-1R C-band SAR SARAL Altimeter/ARGOS OCEANSAT-3 OCM , TIR GISAT MXVNIR/SWIR/ INSAT- 3D TIR/HySI Imager/Sounder EARTH OBSERVATION (LAND AND WATER) RESOURCESAT-1 IMS-1 RESOURCESAT-2 RISAT-1 RESOURCESAT-2A RESOURCESAT-3 RESOURCESAT-3A/3B/3C RISAT-3 GISAT RISAT-1R EARTH OBSERVATION (CARTOGRAPHY) TES CARTOSAT-1 CARTOSAT-2/2A/2B RISAT-1 CARTOSAT-2C/2D CARTOSAT-3 RISAT-3 RISAT-1R EARTH OBSERVATION (ATMOSPHERE & OCEAN) KALPANA-1 INSAT- 3A OCEANSAT-1 INSAT-3D OCEANSAT-2 YOUTHSAT GISAT MEGHA–TROPIQUES OCEANSAT-3 SARAL Current observation capabilities : Optical Payload Sensors in Spatial Res. Swath/ Radiometry Spectral bands Repetivity/ operation Coverage (km) revisit CCD 1 1 Km India & 10 bits 3 (B3, B4, B5) 4 times/ day surround. -
Oih Government of India Department of Space Rajya
OIH GOVERNMENT OF INDIA DEPARTMENT OF SPACE RAJYA SABHA UNSTARRED QUESTION NO. 874 TO BE ANSWERED ON THURSDAY, APRIL 30, 2015 SATELLITE LAUNCHED BY ISRO 874. SHRI RAMDAS ATHAWALE: Will the PRIME MINISTER be pleased to state: (a) the details of the satellites successfully launched so far by ISRO along with those satellites ISRO failed to launch; (b) whether there is any proposal to launch more satellites in near future, if so, the details thereof; and (c) whether Government proposes to enter the global market for images and statistics? ANSWER MINISTER OF STATE IN THE MINISTRY OF PERSONNEL, PG & PENSIONS AND IN THE PRIME MINISTER’S OFFICE (DR. JITENDRA SINGH): (a) As on April 2015, Indian Space Research Organisation (ISRO) has launched 74 satellites. Out of these, 7 satellites failed to reach the orbit due to launch failure and 3 satellites failed in orbit. In addition, ISRO has successfully launched 40 foreign satellites from 19 countries and 4 micro & nano satellites built by students of Indian Universities using Polar Satellite Launch Vehicle (PSLV). The details are enclosed in Annexure-1 (b) Yes, Sir. 6 more satellites are planned to be launched during 2015-16. These are two Communication satellites GSAT-6 & GSAT-15; three Navigation satellites IRNSS-1E, IRNSS-1F & IRNSS-1G; and one Space science satellite ASTROSAT. In addition, it is also planned to launch 13 more satellites from four countries using Polar Satellite Launch Vehicle. The details are enclosed in Annexure-2. …2/- -2- (c) Antrix Corporation Ltd., the commercial arm of Department of Space is already marketing remote sensing data (images) from Indian Remote Sensing satellites in the global market through establishment of International Ground Stations and reseller network. -
25 Years of Indian Remote Sensing Satellite (IRS)
2525 YearsYears ofof IndianIndian RemoteRemote SensingSensing SatelliteSatellite (IRS)(IRS) SeriesSeries Vinay K Dadhwal Director National Remote Sensing Centre (NRSC), ISRO Hyderabad, INDIA 50 th Session of Scientific & Technical Subcommittee of COPUOS, 11-22 Feb., 2013, Vienna The Beginning • 1962 : Indian National Committee on Space Research (INCOSPAR), at PRL, Ahmedabad • 1963 : First Sounding Rocket launch from Thumba (Nov 21, 1963) • 1967 : Experimental Satellite Communication Earth Station (ESCES) established at Ahmedabad • 1969 : Indian Space Research Organisation (ISRO) established (15 August) PrePre IRSIRS --1A1A SatellitesSatellites • ARYABHATTA, first Indian satellite launched in April 1975 • Ten satellites before IRS-1A (7 for EO; 2 Met) • 5 Procured & 5 SLV / ASLV launch SAMIR : 3 band MW Radiometer SROSS : Stretched Rohini Series Satellite IndianIndian RemoteRemote SensingSensing SatelliteSatellite (IRS)(IRS) –– 1A1A • First Operational EO Application satellite, built in India, launch USSR • Carried 4-band multispectral camera (3 nos), 72m & 36m resolution Satellite Launch: March 17, 1988 Baikanur Cosmodrome Kazakhstan SinceSince IRSIRS --1A1A • Established of operational EO activities for – EO data acquisition, processing & archival – Applications & institutionalization – Public services in resource & disaster management – PSLV Launch Program to support EO missions – International partnership, cooperation & global data sets EarlyEarly IRSIRS MultispectralMultispectral SensorsSensors • 1st Generation : IRS-1A, IRS-1B • -
Satish Dhawan: Refractions from Another Time*
SPECIAL SECTION: Satish Dhawan: Refractions from another time* Venkatasubbiah Siddhartha1,† and Yagnaswami Sundara Rajan2 1International Strategic Studies Programme, National Institute of Advanced Studies, Bengaluru 560 012, India 2Former Scientific Secretary ISRO/Former Dr Vikram Sarabhai Distinguished Professor ISRO/DOS, ISRO Headquarters, Bengaluru 560 231, India A preword financial outlays a line item on ‘technology transfer and utilization’. That line item has now grown into the busi- REMINISCING about his time at the California Institute of ness plans of two commercial enterprises of DoS3. Technology (Caltech), USA, the late Sitaram Rao Valluri Accounts by other Indian Space Research Organisation (Director, National Aeronautical Laboratory, NAL), (ISRO) insiders (e.g. refs 4–6) have expatiated in their related to me an occasion when, in a conversation at respective distinctive styles the techno-managerial nitty- Caltech with the legendary Hans Liepmann, the latter gritty of the execution of launch vehicle and satellite pointed to a blackboard with ‘Satish’s writing on it’. programmes of ISRO4–6. Also revealed in them are deci- Liepmann said he had sprayed the board with a transpa- sions made under SD’s watch for the early seeding and rent coating so ‘it could not be rubbed off’. subsequent sprouting of a comprehensive portfolio of ‘Each time I had a difficult decision to make at NAL’, long-gestation enabling technologies and test facilities, Valluri confessed to me, ‘I would ask myself: “Would for liquid propulsion systems in particular. Satish approve?” ’ So, this essay is mostly about my interactions with During its composition, the draft title (‘SD: A Ratna of Dhawan on matters concerning the warp and weft of his Bharat’) of this essay, and several paragraphs drifted into contributions to, and concerns with, the fashioning of the hagiography – albeit sincere. -
History of the Indian Remote Sensing Programme
History of the Indian Remote Sensing Programme Ranganath Navalgund Vikram Sarabhai Distinguished Professor Indian Space Research Organisation Bangalore, India Workshop on Small Satellites & Sensor Technology for Disaster Management, Indo-US S&T Forum CANEUSMarch SSTDM 31, 2014 2014 BEGINNING Stared with the pioneering experiment of detecting Coconut Root Wilt Disease using Color Infrared Film in 1970s by Prof. P. R. Pisharoty. Jun 07,1979 Bhaskara-I (1979) and Bhaskara-II (1981) – Experimental Remote Sensing Satellites provided the Aerial view of Grove Area foundation for the operational Indian Remote Sensing Programme. Nov 20, 1981 (Coconut Root Wilt Disease Study) The Result is operational Indian Remote Sensing Programme with the launch of IRS-1A on March 17, 1988 CANEUS SSTDM 2014 DURING 1980s NRSA established Earth Station Complex at Annaram Village, Shadnagar, 59 km from Balanagar in 1979 to receive Landsat Data TERMINAL-1 (10M DIA) L & S Band 15 Mbps 1980-83: Landsat 2,3 & NOAA- 2, 3 1983-88: Landsat 5, ERS, SPOT & NOAA Today: Multimission ScenarioCANEUS - 4 SSTDMTerminals 2014 (7.5m) - upto 960Mbps EVOLUTION OF (Microwave RISAT-1 (2012) Capability) INDIAN EO SYSTEMS C Band SAR (5.35 GHz) IMS-1 (2008) (Hyperspectral HySI Sensor (64 bands, 506 m) Capability) TWSAT-MX (4 bands, 37 m) TES, Cartosat-1, 2/2A/2B (1999, (High Spatial Resolution 2005, 2007, 2008, 2010) & Stereo Capability) PAN : 2.5 m, 1m Fore +26o Aft: -5o Resourcesat-1/2 (2003, 2011) (Multi resolution, Frequent LISS-3: 23 m, 4 XS, observations, Better LISS-4: 5.8 -
Glimpses of Indian Space Programme
Presentation at the M. V. DHEKANE, International Symposium Associate Director (R&D) in Tokyo, on Vikram Sarabhai Space Centre, Stable use of Outer Space Indian Space Research Organisation 1 during March 3-4, 2016 Trivandrum, India “There are some who question the relevance of space activities in a developing nation. To us, there is no ambiguity of purpose. We are convinced that if we are to play a meaningful role in the comity of nations we should be second to none in the applications of advanced technologies to the real problems of man and Society.” Dr. Vikram A Sarabhai 2 The First Indian Rockets…. Rohini-75 (RH-75) The First rocket made by India and launched from Thumba 20-Nov-1967 Nike-Apache The First sounding rocket launched from Thumba 21-Nov-1963 3 Sounding Rockets 4 ISRO Launch vehicles SLV-3 to GSLV MkIII • GTO Mission • Cryogenics • Maraging Steel, Large Booster • Strap-on Technology • Liquid Propulsion • Closed loop Guidance • Gimbal Control, Flex Nozzle • Onboard RTD • Multiple Satellites injection • Bulbous Heat Shield • Vertical Integration • Solid propulsion • Inertial Systems • Open loop guidance • Orbital Mission GSLV Mk III • Heavy Cryogenics GSLV • Large solid & liquid (2000) Boosters 10000 4500 SLV-3 ASLV PSLV (1994) (1980) (1988) 3000 LEO PAYLOADS (KG) GSLV Mk III Launch Vehicle SLV ASLV PSLV GSLV (Under development) Lift-off weight 17 40 295 450 635 (Tonnes) Payload (kg) 40 (LEO) 150 (LEO) 1600 (SSO) 2000 (GTO) 4000 (GTO) 5 Indian Space programme VISION: Harness space technology for national development, while pursuing -
Indian Remote Sensing Missions
ACKNOWLEDGEMENT This book, “Indian Remote Sensing Missions and Payloads - A Glance” is an attempt to provide in one place the information about all Indian Remote Sensing and scientific missions from Aryabhata to RISAT-1 including some of the satellites that are in the realization phase. This document is compiled by IRS Program Management Engineers from the data available at various sources viz., configuration data books, and other archives. These missions are culmination of the efforts put by all scientists, Engineers, and supporting staff across various centres of ISRO. All their works are duly acknowledged Indian Remote Sensing Missions & Payloads A Glance IRS Programme Management Office Prepared By P. Murugan P.V.Ganesh PRKV Raghavamma Reviewed By C.A.Prabhakar D.L.Shirolikar Approved By Dr.M. Annadurai Program Director, IRS & SSS ISRO Satellite Centre Indian Space Research Organisation Bangalore – 560 017 Table of Contents Sl.No Chapter Name Page No Introduction 1 1 Aryabhata 1.1 2 Bhaskara 1 , 2 2.1 3. Rohini Satellites 3.1 4 IRS 1A & 1B 4.1 5 IRS-1E 5.1 6 IRS-P2 6.1 7 IRS-P3 7.1 8 IRS 1C & 1D 8.1 9 IRS-P4 (Oceansat-1) 9.1 10 Technology Experiment Satellite (TES) 10.1 11 IRS-P6 (ResourceSat-1) 11.1 12 IRS-P5 (Cartosat-1) 12.1 13 Cartosat 2,2A,2B 13.1 14 IMS-1(TWSAT) 14.1 15 Chandrayaan-1 15.1 16 Oceansat-2 16.1 17 Resourcesat-2 17.1 18 Youthsat 18.1 19 Megha-Tropiques 19.1 20 RISAT-1 20.1 Glossary References INTRODUCTION The Indian Space Research Organisation (ISRO) planned a long term Satellite Remote Sensing programme in seventies, and started related activities like conducting field & aerial surveys, design of various types of sensors for aircraft surveys and development of number of application/utilization approaches. -
Access to Space Through Isro Launch Vehicles
Volume -2, Issue-4, October 2012 ACCESS TO SPACE THROUGH ISRO subsystems of a complex launch vehicle but also the maturity attained in conceiving, designing and realizing LAUNCH VEHICLES other vital elements viz., control, guidance, navigation Introduction : and staging systems. The nation’s capability to plan, integrate and carry out a satellite launch mission which is Climbing out of the Earth’s gravity well and transcending truly a multi-disciplinary technological challenge was the dense atmospheric shield is the most energy intensive proved on July 18, 1980 when India successfully orbited crucial first step in the journey into space and the Launch Rohini-1 satellite on SLV-3 E02 flight. Vehicles are the primary viable means of accomplishing this task. India acquired the capability to orbit a satellite While the sub-orbital sounding rockets which just carry in 1980, when SLV-3 the indigenously developed all the payload instruments upto a height of 100 to 200 solid launcher deployed the 40 kg Rohini satellite around kilometers have very few sub-systems apart from the earth. Tremendous progress has been made in this area propulsive device, a Satellite Launcher which has to in the last three decades and today, India is one among import a velocity of around 8 km/sec and precisely the leading space-faring nations with assured access to deliver the payload into a pre targeted injection vector in space through the work-horse operational launcher space has far more complex systems all of which have to PSLV, the Polar Satellite Launch Vehicle. function flawlessly for a successful orbital mission. -
India's Early Satellites – Spin-Stabilized and Bias Momentum
India’s Early Satellites – Spin-Stabilized and Bias Momentum ISRO Aryabhata – for Space Science (Launch date 19 April 1975) Aryabhata was India's first satellite It was launched by the Soviet Union from Kapustin Yar Mission type Astrophysics Satellite of Earth Aryabhata was built by the ISRO Launch date 19 April 1975 engineers to conduct Carrier rocket Cosmos-3M experiments related to X-ray astronomy, solar physics, and Mass 360.0 kg Power 46 W from solar panels aeronomy. Orbital elements Regime LEO The satellite reentered the Inclination 50.7º Orbital period 96 minutes Earth's atmosphere on 11 Apoapsis 619 km February 1992. Periapsis 563 km *National Space Science Data Center, NASA Goddard Space Flight Center Bhaskara (Earth Observation) Satellites (launched in 1979-1981)* Bhaskara-I and II Satellites were built by the ISRO, and they were India's first low orbit Earth Observation Satellite.They collected data on telemetry, oceanography, hydrology. Bhaskara-I, weighing 444 kg at launch, was launched on June 7, 1979 from Kapustin Yar aboard the Intercosmos launch vehicle. It was placed in an orbital Perigee of 394 km and Apogee of 399 km at an inclination of 50.7°. The satellite consisted of- Two television cameras operating in visible (0.6 micrometre) and near-infrared (0.8 micrometre) and collected data related to hydrology, forestry and geology. Satellite microwave radiometer (SAMIR) operating at 19 GHz and 22 GHz for study of ocean-state, water vapor, liquid water content in the atmosphere, etc. The satellite provided ocean and land surface data. Housekeeping telemetry was received until re-entry on 17 February 1989. -
NISAR Science Workshop – 2014
Science Workshop – 2014 NISAR Space Applications Centre NISAR Mission Overview Tapan Misra (ISRO) & Paul Rosen (JPL) Space Applications Centre (SAC) NASA ISRO Synthetic Aperture Radar (NISAR) NISAR Mission Overview Payload / Mission Characteristics Would Enable 1 L-band (24 cm wavelength) Low temporal decorrelation and foliage penetration 2 S-band (12 cm wavelength) Sensitivity to light vegetation 3 SweepSAR technique with Imaging Swath > Global data collection 240 km 4 Polarimetry (Single/Dual/Quad) Surface characterization and biomass estimation 5 12-day exact repeat Rapid Sampling 6 3 – 10 meters mode-dependent SAR resolution Small-scale observations 7 3 years science operations (5 years Time-series analysis consumables) 8 Pointing control < 273 arcseconds Deformation interferometry 9 Orbit control < 500 meters Deformation interferometry 10 > 30% observation duty cycle Complete land/ice coverage 11 Left/Right pointing capability Polar coverage, north and south th th *Mission Concept – Pre-decisional – for Planning and NISAR Science Workshop, SAC Ahmedabad – 17 & 18 Nov. 2014 2 Discussion Purposes Only Key Capabilities for NISAR Repeatable orbits and instrument pointing Swath width sufficient to cover ground-track spacing at equator Polarimetric synthetic aperture radar with “industry-standard” performance parameters valid over the full swath All imaging with the instrument boresight pointed 37 degrees off-nadir and +/- 90 degrees off the body-fixed velocity vector Orbit reconstruction to cm-scale accuracy for efficient interferometric processing and calibration Sufficient duty cycle and mission resources to strobe Earth’s land and ice on ascending and descending orbits each repeat cycle 24-hour turnaround on urgent retargeting and 5-hour latency for data designated as urgent th th *Mission Concept – Pre-decisional – for Planning and NISAR Science Workshop, SAC Ahmedabad – 17 & 18 Nov.