The mangalyaan (after mission completion)
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The document summarizes India's Mars Orbiter Mission (MOM) launched in 2013. MOM's objectives were to demonstrate India's technological capability to design, plan, manage and operate an interplanetary mission at a low cost. It carried scientific instruments to study Mars' surface, morphology, atmosphere and assess if conditions were ever suitable for life. The mission successfully placed the Mars orbiter into orbit in 2014, making India the first Asian nation and fourth space agency globally to reach Mars. The entire mission cost approximately 450 crore INR ($63 million USD).
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Mangalyaan (India's mission to mars)
India's Mars Orbiter Mission (MOM), also known as Mangalyaan, is the cheapest Mars mission ever at a cost of about $74 million. It was developed and launched in just 15 months and involves sending an orbiter craft to orbit Mars and study its surface features and atmosphere. The mission aims to demonstrate India's technological capability to design, plan and manage deep space missions.
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Mars Mission of india (MANGALYAN)
India launched its first mission to Mars, called MOM or Mars Orbiter Mission, on November 5, 2013. The mission objectives were to develop technologies for designing, planning and operating interplanetary missions, and to study the Martian surface, atmosphere and climate. The Mars Orbiter spacecraft was launched using the Polar Satellite Launch Vehicle. It weighed 1.35 tons and cost $73 million. After traveling 300 days, it successfully entered orbit around Mars, making India the fifth space agency to do so. The orbiter carried scientific instruments to study Mars' morphology, topography, mineralogy and atmosphere. While some saw the mission as putting India among the leading space-faring nations, others criticized the large cost when India faces
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This document summarizes several planetary exploration missions. It discusses Chandrayaan-1, India's first lunar orbiter mission, and its objectives to map lunar minerals and terrain. It also discusses NASA's MAVEN and Curiosity missions to Mars, with MAVEN studying the Martian atmosphere and Curiosity analyzing samples to search for evidence of past life. Additionally, it summarizes Cassini's ongoing mission in orbit around Saturn, making discoveries about the rings and moons like Titan and Enceladus.
mangalyaan
The Mars Orbital Mission (MOM) aims to design and realize an orbiter with the capability to survive Earth maneuvers, a 300-day cruise phase, Mars orbit insertion and on-orbit phases around Mars to study its surface features, mineralogy and atmosphere. The objectives include deep space communication and navigation with autonomous capabilities. The total cost of 450 crore rupees for MOM is less than 1/10th of the amount spent by NASA on its MAVEN Mars mission. MOM was launched aboard the PSLV rocket on November 5th, 2013 and includes scientific instruments to study Mars' composition, atmosphere and climate.
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Mars Mission of india (MANGALYAN)
India launched its first mission to Mars, called MOM or Mars Orbiter Mission, on November 5, 2013. The mission objectives were to develop technologies for designing, planning and operating interplanetary missions, and to study the Martian surface, atmosphere and climate. The Mars Orbiter spacecraft was launched using the Polar Satellite Launch Vehicle. It weighed 1.35 tons and cost $73 million. After traveling 300 days, it successfully entered orbit around Mars, making India the fifth space agency to do so. The orbiter carried scientific instruments to study Mars' morphology, topography, mineralogy and atmosphere. While some saw the mission as putting India among the leading space-faring nations, others criticized the large cost when India faces
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mangalyaan
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The Mars Orbiter Mission was launched by ISRO on November 5, 2013 from Sriharikota, India. Its primary objective was to demonstrate India's ability to design, plan and manage an interplanetary mission. The spacecraft weighed 1350 kg at launch and successfully performed orbit raising maneuvers before the Trans-Mars Injection on November 30th, 2013 that placed it on a heliocentric orbit en route to Mars. The orbiter is scheduled to perform Mars Orbit Insertion on September 24, 2014 to study the Martian surface, atmosphere and further demonstrate India's deep space capabilities.
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The Mars Orbiter Mission (MOM), also known as Mangalyaan, is India's first interplanetary mission, which aims to demonstrate technologies required for designing and operating an orbiter mission to Mars. Launched in 2013 aboard a Polar Satellite Launch Vehicle from Sriharikota, India, MOM entered orbit around Mars in 2014, making India the first Asian nation to reach Mars. The mission carries scientific instruments to study the Martian surface, atmosphere and climate. If successful, MOM will make India the fourth space agency to place a spacecraft in orbit around Mars.
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The document discusses India's Mars Orbiter Mission (MOM) launched in 2013, which successfully entered Mars' orbit in 2014, making India the first nation to reach Mars on its maiden attempt. Key details include:
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- After a 298-day transit, MOM successfully entered Mars' orbit on September 24, 2014, making India the fourth space agency to reach Mars.
- The mission demonstrates India's capabilities for interplanetary travel while advancing scientific understanding of Mars through its onboard instruments.
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The document discusses ISRO's Mars Orbiter Mission (MOM) which was completed at a very low cost of $73 million compared to other Mars missions. Some key reasons for the low cost included a simple design using homegrown technology, long working hours of engineers, low labor costs in India, and efficient time management. The mission was also fast-tracked and completed within a record 15 months. ISRO used public-private partnerships and worked with 170 domestic industries to outsource parts of the mission. This collaborative approach helped lower costs significantly.
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The document provides an overview of India's Mars Orbiter Mission (MOM). [1] The primary objectives were to demonstrate India's low-cost capabilities for interplanetary travel and explore the Martian surface and atmosphere. [2] MOM successfully entered Mars' orbit in 2014, making India the first nation to do so on its first attempt. [3] The mission achieved its goals of technological development and scientific exploration of Mars through onboard instruments, with a total cost of only $71 million.
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The document summarizes India's Mars Orbiter Mission (MOM). It describes the objectives of studying Mars' climate, atmosphere and potential for life. MOM was launched in 2013 using the PSLV rocket and placed the spacecraft in Martian orbit in 2014. The orbiter carries instruments to analyze Mars' atmosphere and surface composition. It aims to demonstrate India's low-cost spaceflight capabilities and further scientific understanding of Mars on a smaller budget than other Mars missions. MOM has exceeded its original mission duration and continues to operate successfully from Martian orbit, collecting data to study the Red Planet.
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The document discusses India's Mars Orbiter Mission (MOM), known as Mangalyaan, which was launched by the Indian Space Research Organisation (ISRO) in November 2013 with the goal of placing an orbiter around Mars to study its surface, atmosphere and climate. ISRO's MOM mission aims to demonstrate India's low-cost spaceflight capabilities and technological prowess. The orbiter successfully entered Mars' orbit in September 2014, making India the first nation to reach Mars on its first attempt and the first nation to successfully place an orbiter around Mars on its maiden interplanetary mission.
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- The mission achieved India's goal of successful Mars orbital insertion
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- It describes the 8 phases of MOM, from launch on the PSLV rocket to orbital insertion around Mars in September 2014.
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- The mission achieved India's goal of successful Mars orbital insertion
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India successfully launched its first interplanetary mission, called Mangalyaan, to Mars on November 5, 2013. The mission chairman exclaimed that the spacecraft had reached its intended elliptical orbit around Mars and was in good health. The success of this mission makes India the fourth country to send a spacecraft to Mars, demonstrating its technological capabilities and boosting national pride. The Mars Orbiter Mission, also known as Mangalyaan, aims to develop technologies for designing, planning, and operating an interplanetary mission, and will study Mars' atmosphere, surface features, and mineralogy using scientific instruments onboard.
Mars orbitar misson [mom]
The Mars Orbiter Mission (MOM) was India's first interplanetary mission, launched in 2013. It successfully entered Mars' orbit in 2014, making India the first nation to reach Mars on its maiden attempt. MOM's objectives were to demonstrate India's technological capability for interplanetary travel and conduct scientific studies of Mars' surface and atmosphere. It carried instruments to analyze Mars' atmosphere, surface, and particle environment. After several orbit raising maneuvers, MOM successfully inserted into Mars orbit and remains operational, far exceeding its intended lifespan.
Mangalyaan
India successfully launched the Mars Orbiter Mission (MOM) spacecraft, also called Mangalyaan, and inserted it into orbit around Mars. MOM was India's first interplanetary mission and made India the fourth space agency to reach Mars, after NASA, Russian, and European space agencies. The mission cost approximately $74 million, making it one of the least expensive Mars missions to date. Over the course of several months, MOM performed a series of orbit raising maneuvers and engine burns to break free from Earth's gravity and enter a heliocentric orbit en route to Mars before successfully being captured by Mars' gravity in September 2014.
INDIA'S MARS ORBITER MISSION
The document discusses India's Mars Orbiter Mission (MOM) launched in 2013. MOM's objectives were to develop technologies for designing and operating an interplanetary mission, and to explore Mars' surface, atmosphere, and mineralogy using scientific instruments. The mission cost 4.54 billion rupees total. MOM's spacecraft weighed 1350 kg and carried 5 scientific payloads. It was successfully launched on November 5, 2013 and entered Mars' orbit on September 24, 2014, making India the first Asian nation to reach Mars.
Mars orbiter mission
The document summarizes India's Mars Orbiter Mission (MOM) launched in 2013. It describes Mars and previous Mars missions by other countries. MOM was India's first interplanetary mission, making it the fourth space agency to reach Mars. The mission's objectives were to demonstrate India's low-cost space technology and study Mars' surface features and atmosphere. MOM carried scientific instruments that analyzed Mars' atmosphere and surface composition, and it remains operational in Mars' orbit. The successful mission boosted India's presence in space exploration and scientific research.
MOM Mission
ISRO was established in 1969 to oversee India's space program. Some key accomplishments include launching India's first satellite in 1975 and developing launch vehicles like PSLV and GSLV. In 2008, ISRO successfully launched Chandrayaan-1, India's first lunar mission. On November 5, 2013, ISRO launched the Mars Orbiter Mission (MOM), its first interplanetary mission, which is currently orbiting Mars and gathering scientific data. The mission aims to demonstrate India's capability for interplanetary travel through technological objectives like designing a Mars orbiter and navigating in deep space, as well as scientific objectives like studying Mars' surface and atmosphere.
Mars Orbiter Mission (MOM), also called Mangalyaan With Mp4 Video..best ppt
The Mars Orbiter Mission (MOM), also called Mangalyaan ("Mars-craft" from Sanskrit मंगल mangala, "Mars" and यान yāna, "craft, vehicle"), is a spacecraft orbiting Mars since 24 September 2014. It was launched on 5 November 2013 by the Indian Space Research Organisation (ISRO)
Mangalyaan by Ashwin.pptx
India's Mangalyaan Mars Orbiter Mission was launched on November 5, 2013 by the Indian Space Research Organisation (ISRO). The spacecraft successfully entered Mars' orbit on September 24, 2014, making ISRO the fourth space agency to achieve Mars orbit. The Mars Orbiter Mission's objectives were to develop the technologies required for interplanetary missions and to study the Martian surface and atmosphere. Key people involved in the mission included K. Radhakrishnan, Mylswamy Annadurai, and P. Kunhikrishnan.
Mangalayan
The MARS orbiter mission called "MANGALYAAN" is India's first mission to Mars, launched from Sriharikota, AP. If successful, ISRO would become the fourth space agency to reach Mars. The mission aims to develop technology for designing, planning, managing and operating interplanetary missions. It will study Mars' atmosphere and surface using five instruments onboard. After leaving Earth, the spacecraft will cruise for 10 months before entering Mars' orbit in September 2014 to analyze the surface and atmosphere, including searching for methane using a methane sensor.
Indian Mars Orbiter Mission
This presentation gives inforamation about the indian mars orbiter mission's objectives, it's launchpad, payload, it's tracking system ,budjet etc.
Space research:OUTLINE,HISTORY AND PROGRESS
Space research involves scientific studies carried out in outer space using scientific equipment. It includes various disciplines like Earth science, materials science, biology, medicine, and physics. Space research emerged after World War II based on advancing rocket technology and includes fields like earth observations, geodesy, space physics, planetology, astronomy, materials sciences, life sciences, and physics. Some notable space research missions and satellites include the Upper Atmosphere Research Satellite, International Gamma-Ray Astrophysics Laboratory, Hubble Space Telescope, Salyut 1, Skylab, and Mir space stations. India has also made significant contributions to space research through organizations like ISRO.
National Income of India is given in this video
This document provides information about the Indian Space Research Organisation (ISRO). It discusses the history and establishment of ISRO in 1969. It outlines some of ISRO's key achievements including the development of satellite launch vehicles, missions to study planets like Mars and the Moon, establishing satellite systems for communications, earth observation, and navigation. It also discusses future planned missions and challenges facing India's space program.
mars orbitter mission success
This document provides information about the Mars Orbiter Mission (MOM) launched by India's space agency ISRO. MOM's objectives were to develop the technologies to design, plan, manage and operate an interplanetary mission; place a satellite in Mars orbit; and study the Martian surface, morphology, mineralogy and atmosphere. The spacecraft was launched in 2013 aboard an ISRO PSLV rocket and entered Mars orbit in 2014. Its scientific payload included instruments to study atmospheric composition, methane, temperature and mineralogy. The mission successfully demonstrated India's low-cost Mars orbital insertion capabilities.
Mars Mission
This document provides information about a homework assignment submitted by Kartikey Agarwal about the Mars Orbiter Mission (MOM). It discusses key details of MOM including its objectives to study Mars' surface features, morphology, and atmosphere. It describes the spacecraft's launch via the PSLV rocket and successful orbital insertion around Mars in September 2014. The document also outlines the scientific payloads onboard MOM to analyze Mars' atmosphere and surface composition.
Harshil gaurang
Mangalyaan, also known as the Mars Orbiter Mission (MOM), was India's first interplanetary mission. It was launched by the Indian Space Research Organization (ISRO) on November 5, 2013, and successfully entered Mars' orbit on September 24, 2014, making India the first nation to succeed on its first attempt. The mission's objectives were to develop the technologies required for designing, planning, management and operations of an interplanetary mission, and to help better understand the Martian surface and atmosphere. Key personnel involved included K. Radhakrishnan, chairman of ISRO, M. Annadurai, programme director of MOM, and S. Ramakrishnan, director
Mom
Mangalyaan was India's first interplanetary mission, which successfully entered Mars' orbit on September 24, 2014. The Mars Orbiter Mission (MOM) launched on November 5, 2013 with the goal of demonstrating India's technological capability to design, plan and manage an interplanetary mission. MOM carried scientific instruments to study the Martian surface, atmosphere and mineral composition. Its mission objectives included developing key technologies for future Mars missions and exploring Mars through indigenous scientific payloads.
Isro’s mars orbiter mission
ISRO was formed in 1969 by India's first prime minister Jawaharlal Nehru to advance India's space science research. ISRO's first interplanetary mission was the Mars Orbiter Mission (MOM) launched in 2013, which made India the first nation to successfully reach Mars orbit on its first attempt. MOM's objectives were to study the Martian surface, atmosphere, and moons using onboard instruments in order to help understand the Red Planet and India's capabilities for future space exploration.
MARS ORBITER MISSION (MOM) (MANGALYAN)
The document summarizes India's Mars Orbiter Mission (MOM), which made India the first nation to successfully reach Mars on its first attempt. MOM was launched aboard a Polar Satellite Launch Vehicle on November 5, 2013. It carried scientific instruments to study the Martian atmosphere and surface. After orbit raising maneuvers, MOM was successfully inserted into Mars' orbit on September 24, 2014, making India the fourth space agency to reach Mars. The mission aims to develop technologies for interplanetary travel and explore the Red Planet's features and atmosphere.
Marsh orbitar mission 1
The Mars Orbitary Mission document summarizes India's first interplanetary mission to Mars. The objectives were to demonstrate India's rocket and spacecraft capabilities, explore Mars' surface and atmosphere, and incorporate autonomous features. The spacecraft carried five scientific payloads and successfully launched in November 2013. After a series of maneuvers, it entered Mars' orbit in September 2014, making India the first nation to complete a Mars mission on its first attempt. The mission achieved valuable scientific data collection and experience for future collaborations.
Similar to The mangalyaan (after mission completion) (20)
Mars Orbiter Mission (MOM), also called Mangalyaan With Mp4 Video..best ppt
Mars Orbiter Mission (MOM), also called Mangalyaan With Mp4 Video..best ppt
More from Akhilesh Rathiya
Controlling system of Turbine
This document discusses the need for control of various parameters in a steam power plant and describes the types of sensors used to monitor and control these parameters. Temperature, pressure, level, flow, and RPM must be carefully controlled to prevent damage to equipment and ensure safe operation. Thermocouples and RTDs are used to measure boiler and economizer temperatures. Bourdon tubes and high-precision digital sensors monitor boiler and condenser pressures. Level sensors detect substance levels in tanks. A rotor sensor measures steam flow rate. An AM4096 sensor monitors turbine shaft RPM to less than 0.1 degree accuracy. Proper monitoring and control of these parameters is essential for safe, efficient operation of the plant.
RHEINMETALL AUTMOTIVE: A Piston Manufacturing Company
This document contains information about KSPG Automotive India Private Limited, including:
1. KSPG Automotive India Private Limited manufactures auto components such as exhaust gas recirculating valves, pistons, and vacuum pumps for customers like BMW, General Motors, Volkswagen, Renault, and Mahindra.
2. The company was formerly known as Pierburg India Private Limited and is located in Pune, India, operating as a subsidiary of Pierburg GmbH.
3. KSPG Automotive India Private Limited benefits from technical support from a number of qualified engineers located in Pune, as well as a local supplier base that provides quality components globally.
Wiseco Piston Manufacturing Company
The document provides information about Wiseco Piston Company, including its history, facilities, organization structure, and production process. It was established in 1940 in Cleveland, Ohio and has since expanded to over 150,000 square feet with facilities in the US, Canada, and Europe. The plant layout section describes its 200 acre facility in Industrial Park Boulevard, Ohio which houses various operations like piston, ring, and casting production. The organization chart shows the management structure and process flow chart outlines the material selection process for testing and characterizing materials.
Rolex Wrist Watch production management lab by akshay sinha
This document provides information about Rolex, including its history, locations, manufacturing processes, and materials. It was founded in 1905 in London and moved to Geneva in 1919. Rolex produces about 2,000 watches per day at its facilities. Its largest location is in Bienne, Switzerland, where it has proprietary machines that manufacture unique components. The production process involves idea development, prototyping, manufacturing, delivery, and support. Rolex uses high-quality materials like stainless steel, gold, and ceramics in its watches and develops these materials and production processes in-house to ensure quality and durability.
Bhilai steel plant plate mill & mars 1
The document is a vocational training report summarizing Akhilesh Paikra's training at Bhilai Steel Plant. It provides an overview of Steel Authority of India Limited (SAIL) and Bhilai Steel Plant, including their production processes. It describes the plant's raw materials, major production areas like the plate mill, and achievements. The training covered safety practices, production workflows, and equipment in different areas of the large integrated steelmaking facility.
The Knuckle Joint Assembly
The document details the design of a knuckle joint to transmit 150kN of force while meeting various design stress limits. Mathematical calculations are shown to determine the optimal diameters and thicknesses for the rod, pin, eye, and fork components to prevent failure under tensile, compressive, shear, and crushing stresses. The final dimensions selected are: rod diameter of 48.86mm, pin diameter of 43.7mm, outer eye diameter of 97.72mm, eye thickness of 61.075mm, and fork thickness of 36.64mm. Diagrams of the knuckle joint assembly and its components are provided.
Auto mobile engineering
The document provides information about various components of an automobile. It discusses the chassis, axles, suspension system, tires, braking system, steering system, transmission system including the clutch, gearbox and propeller shaft. It also covers the engine, intake manifold, carburetor and different types of engines. The document categorizes automobiles and defines key terms like chassis, axle, suspension and others.
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TOPIC OF DISCUSSION: CENTRIFUGATION SLIDESHARE.pptx
Centrifugation is a powerful technique used in laboratories to separate components of a heterogeneous mixture based on their density. This process utilizes centrifugal force to rapidly spin samples, causing denser particles to migrate outward more quickly than lighter ones. As a result, distinct layers form within the sample tube, allowing for easy isolation and purification of target substances.
Describing and Interpreting an Immersive Learning Case with the Immersion Cub...
Current descriptions of immersive learning cases are often difficult or impossible to compare. This is due to a myriad of different options on what details to include, which aspects are relevant, and on the descriptive approaches employed. Also, these aspects often combine very specific details with more general guidelines or indicate intents and rationales without clarifying their implementation. In this paper we provide a method to describe immersive learning cases that is structured to enable comparisons, yet flexible enough to allow researchers and practitioners to decide which aspects to include. This method leverages a taxonomy that classifies educational aspects at three levels (uses, practices, and strategies) and then utilizes two frameworks, the Immersive Learning Brain and the Immersion Cube, to enable a structured description and interpretation of immersive learning cases. The method is then demonstrated on a published immersive learning case on training for wind turbine maintenance using virtual reality. Applying the method results in a structured artifact, the Immersive Learning Case Sheet, that tags the case with its proximal uses, practices, and strategies, and refines the free text case description to ensure that matching details are included. This contribution is thus a case description method in support of future comparative research of immersive learning cases. We then discuss how the resulting description and interpretation can be leveraged to change immersion learning cases, by enriching them (considering low-effort changes or additions) or innovating (exploring more challenging avenues of transformation). The method holds significant promise to support better-grounded research in immersive learning.
Mechanisms and Applications of Antiviral Neutralizing Antibodies - Creative B...
Neutralizing antibodies, pivotal in immune defense, specifically bind and inhibit viral pathogens, thereby playing a crucial role in protecting against and mitigating infectious diseases. In this slide, we will introduce what antibodies and neutralizing antibodies are, the production and regulation of neutralizing antibodies, their mechanisms of action, classification and applications, as well as the challenges they face.
Male reproduction physiology by Suyash Garg .pptx
Physiology of Male reproduction.
Video mentioned at page no. 23 as summary for better understanding
JAMES WEBB STUDY THE MASSIVE BLACK HOLE SEEDS
The pathway(s) to seeding the massive black holes (MBHs) that exist at the heart of galaxies in the present and distant Universe remains an unsolved problem. Here we categorise, describe and quantitatively discuss the formation pathways of both light and heavy seeds. We emphasise that the most recent computational models suggest that rather than a bimodal-like mass spectrum between light and heavy seeds with light at one end and heavy at the other that instead a continuum exists. Light seeds being more ubiquitous and the heavier seeds becoming less and less abundant due the rarer environmental conditions required for their formation. We therefore examine the different mechanisms that give rise to different seed mass spectrums. We show how and why the mechanisms that produce the heaviest seeds are also among the rarest events in the Universe and are hence extremely unlikely to be the seeds for the vast majority of the MBH population. We quantify, within the limits of the current large uncertainties in the seeding processes, the expected number densities of the seed mass spectrum. We argue that light seeds must be at least 103 to 105 times more numerous than heavy seeds to explain the MBH population as a whole. Based on our current understanding of the seed population this makes heavy seeds (Mseed > 103 M⊙) a significantly more likely pathway given that heavy seeds have an abundance pattern than is close to and likely in excess of 10−4 compared to light seeds. Finally, we examine the current state-of-the-art in numerical calculations and recent observations and plot a path forward for near-future advances in both domains.
Sustainable Land Management - Climate Smart Agriculture
Sustainable Land Management - Climate Smart AgricultureInternational Food Policy Research Institute- South Asia Office
PPT on Sustainable Land Management presented at the three-day 'Training and Validation Workshop on Modules of Climate Smart Agriculture (CSA) Technologies in South Asia' workshop on April 22, 2024.
The cost of acquiring information by natural selection
This is a short talk that I gave at the Banff International Research Station workshop on Modeling and Theory in Population Biology. The idea is to try to understand how the burden of natural selection relates to the amount of information that selection puts into the genome.
It's based on the first part of this research paper:
The cost of information acquisition by natural selection
Ryan Seamus McGee, Olivia Kosterlitz, Artem Kaznatcheev, Benjamin Kerr, Carl T. Bergstrom
bioRxiv 2022.07.02.498577; doi: https://doi.org/10.1101/2022.07.02.498577
Discovery of An Apparent Red, High-Velocity Type Ia Supernova at 𝐳 = 2.9 wi...
We present the JWST discovery of SN 2023adsy, a transient object located in a host galaxy JADES-GS
+
53.13485
−
27.82088
with a host spectroscopic redshift of
2.903
±
0.007
. The transient was identified in deep James Webb Space Telescope (JWST)/NIRCam imaging from the JWST Advanced Deep Extragalactic Survey (JADES) program. Photometric and spectroscopic followup with NIRCam and NIRSpec, respectively, confirm the redshift and yield UV-NIR light-curve, NIR color, and spectroscopic information all consistent with a Type Ia classification. Despite its classification as a likely SN Ia, SN 2023adsy is both fairly red (
�
(
�
−
�
)
∼
0.9
) despite a host galaxy with low-extinction and has a high Ca II velocity (
19
,
000
±
2
,
000
km/s) compared to the general population of SNe Ia. While these characteristics are consistent with some Ca-rich SNe Ia, particularly SN 2016hnk, SN 2023adsy is intrinsically brighter than the low-
�
Ca-rich population. Although such an object is too red for any low-
�
cosmological sample, we apply a fiducial standardization approach to SN 2023adsy and find that the SN 2023adsy luminosity distance measurement is in excellent agreement (
≲
1
�
) with
Λ
CDM. Therefore unlike low-
�
Ca-rich SNe Ia, SN 2023adsy is standardizable and gives no indication that SN Ia standardized luminosities change significantly with redshift. A larger sample of distant SNe Ia is required to determine if SN Ia population characteristics at high-
�
truly diverge from their low-
�
counterparts, and to confirm that standardized luminosities nevertheless remain constant with redshift.
Randomised Optimisation Algorithms in DAPHNE
Slides from talk:
Aleš Zamuda: Randomised Optimisation Algorithms in DAPHNE .
Austrian-Slovenian HPC Meeting 2024 – ASHPC24, Seeblickhotel Grundlsee in Austria, 10–13 June 2024
https://ashpc.eu/
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Targeting Hsp90 and its pathogen Orthologs with Tethered Inhibitors as a Diagnostic and Therapeutic Strategy for cancer and infectious diseases with Dr. Timothy Haystead.Pests of Storage_Identification_Dr.UPR.pdf
InIndia-post-harvestlosses-unscientificstorage,insects,rodents,micro-organismsetc.,accountforabout10percentoftotalfoodgrains
Graininfestation
Directdamage
Indirectly
•theexuviae,skin,deadinsects
•theirexcretawhichmakefoodunfitforhumanconsumption
About600speciesofinsectshavebeenassociatedwithstoredgrainproducts
100speciesofinsectpestsofstoredproductscauseeconomiclosses
Signatures of wave erosion in Titan’s coasts
The shorelines of Titan’s hydrocarbon seas trace flooded erosional landforms such as river valleys; however, it isunclear whether coastal erosion has subsequently altered these shorelines. Spacecraft observations and theo-retical models suggest that wind may cause waves to form on Titan’s seas, potentially driving coastal erosion,but the observational evidence of waves is indirect, and the processes affecting shoreline evolution on Titanremain unknown. No widely accepted framework exists for using shoreline morphology to quantitatively dis-cern coastal erosion mechanisms, even on Earth, where the dominant mechanisms are known. We combinelandscape evolution models with measurements of shoreline shape on Earth to characterize how differentcoastal erosion mechanisms affect shoreline morphology. Applying this framework to Titan, we find that theshorelines of Titan’s seas are most consistent with flooded landscapes that subsequently have been eroded bywaves, rather than a uniform erosional process or no coastal erosion, particularly if wave growth saturates atfetch lengths of tens of kilometers.
MICROBIAL INTERACTION PPT/ MICROBIAL INTERACTION AND THEIR TYPES // PLANT MIC...
MICROBIAL INTERACTION PPT/ MICROBIAL INTERACTION AND THEIR TYPES // PLANT MIC...ABHISHEK SONI NIMT INSTITUTE OF MEDICAL AND PARAMEDCIAL SCIENCES , GOVT PG COLLEGE NOIDA
Microbial interaction
Microorganisms interacts with each other and can be physically associated with another organisms in a variety of ways.
One organism can be located on the surface of another organism as an ectobiont or located within another organism as endobiont.
Microbial interaction may be positive such as mutualism, proto-cooperation, commensalism or may be negative such as parasitism, predation or competition
Types of microbial interaction
Positive interaction: mutualism, proto-cooperation, commensalism
Negative interaction: Ammensalism (antagonism), parasitism, predation, competition
I. Mutualism:
It is defined as the relationship in which each organism in interaction gets benefits from association. It is an obligatory relationship in which mutualist and host are metabolically dependent on each other.
Mutualistic relationship is very specific where one member of association cannot be replaced by another species.
Mutualism require close physical contact between interacting organisms.
Relationship of mutualism allows organisms to exist in habitat that could not occupied by either species alone.
Mutualistic relationship between organisms allows them to act as a single organism.
Examples of mutualism:
i. Lichens:
Lichens are excellent example of mutualism.
They are the association of specific fungi and certain genus of algae. In lichen, fungal partner is called mycobiont and algal partner is called
II. Syntrophism:
It is an association in which the growth of one organism either depends on or improved by the substrate provided by another organism.
In syntrophism both organism in association gets benefits.
Compound A
Utilized by population 1
Compound B
Utilized by population 2
Compound C
utilized by both Population 1+2
Products
In this theoretical example of syntrophism, population 1 is able to utilize and metabolize compound A, forming compound B but cannot metabolize beyond compound B without co-operation of population 2. Population 2is unable to utilize compound A but it can metabolize compound B forming compound C. Then both population 1 and 2 are able to carry out metabolic reaction which leads to formation of end product that neither population could produce alone.
Examples of syntrophism:
i. Methanogenic ecosystem in sludge digester
Methane produced by methanogenic bacteria depends upon interspecies hydrogen transfer by other fermentative bacteria.
Anaerobic fermentative bacteria generate CO2 and H2 utilizing carbohydrates which is then utilized by methanogenic bacteria (Methanobacter) to produce methane.
ii. Lactobacillus arobinosus and Enterococcus faecalis:
In the minimal media, Lactobacillus arobinosus and Enterococcus faecalis are able to grow together but not alone.
The synergistic relationship between E. faecalis and L. arobinosus occurs in which E. faecalis require folic acid
Evidence of Jet Activity from the Secondary Black Hole in the OJ 287 Binary S...
Wereport the study of a huge optical intraday flare on 2021 November 12 at 2 a.m. UT in the blazar OJ287. In the binary black hole model, it is associated with an impact of the secondary black hole on the accretion disk of the primary. Our multifrequency observing campaign was set up to search for such a signature of the impact based on a prediction made 8 yr earlier. The first I-band results of the flare have already been reported by Kishore et al. (2024). Here we combine these data with our monitoring in the R-band. There is a big change in the R–I spectral index by 1.0 ±0.1 between the normal background and the flare, suggesting a new component of radiation. The polarization variation during the rise of the flare suggests the same. The limits on the source size place it most reasonably in the jet of the secondary BH. We then ask why we have not seen this phenomenon before. We show that OJ287 was never before observed with sufficient sensitivity on the night when the flare should have happened according to the binary model. We also study the probability that this flare is just an oversized example of intraday variability using the Krakow data set of intense monitoring between 2015 and 2023. We find that the occurrence of a flare of this size and rapidity is unlikely. In machine-readable Tables 1 and 2, we give the full orbit-linked historical light curve of OJ287 as well as the dense monitoring sample of Krakow.
Candidate young stellar objects in the S-cluster: Kinematic analysis of a sub...
Context. The observation of several L-band emission sources in the S cluster has led to a rich discussion of their nature. However, a definitive answer to the classification of the dusty objects requires an explanation for the detection of compact Doppler-shifted Brγ emission. The ionized hydrogen in combination with the observation of mid-infrared L-band continuum emission suggests that most of these sources are embedded in a dusty envelope. These embedded sources are part of the S-cluster, and their relationship to the S-stars is still under debate. To date, the question of the origin of these two populations has been vague, although all explanations favor migration processes for the individual cluster members. Aims. This work revisits the S-cluster and its dusty members orbiting the supermassive black hole SgrA* on bound Keplerian orbits from a kinematic perspective. The aim is to explore the Keplerian parameters for patterns that might imply a nonrandom distribution of the sample. Additionally, various analytical aspects are considered to address the nature of the dusty sources. Methods. Based on the photometric analysis, we estimated the individual H−K and K−L colors for the source sample and compared the results to known cluster members. The classification revealed a noticeable contrast between the S-stars and the dusty sources. To fit the flux-density distribution, we utilized the radiative transfer code HYPERION and implemented a young stellar object Class I model. We obtained the position angle from the Keplerian fit results; additionally, we analyzed the distribution of the inclinations and the longitudes of the ascending node. Results. The colors of the dusty sources suggest a stellar nature consistent with the spectral energy distribution in the near and midinfrared domains. Furthermore, the evaporation timescales of dusty and gaseous clumps in the vicinity of SgrA* are much shorter ( 2yr) than the epochs covered by the observations (≈15yr). In addition to the strong evidence for the stellar classification of the D-sources, we also find a clear disk-like pattern following the arrangements of S-stars proposed in the literature. Furthermore, we find a global intrinsic inclination for all dusty sources of 60 ± 20◦, implying a common formation process. Conclusions. The pattern of the dusty sources manifested in the distribution of the position angles, inclinations, and longitudes of the ascending node strongly suggests two different scenarios: the main-sequence stars and the dusty stellar S-cluster sources share a common formation history or migrated with a similar formation channel in the vicinity of SgrA*. Alternatively, the gravitational influence of SgrA* in combination with a massive perturber, such as a putative intermediate mass black hole in the IRS 13 cluster, forces the dusty objects and S-stars to follow a particular orbital arrangement. Key words. stars: black holes– stars: formation– Galaxy: center– galaxies: star formation
ESA/ACT Science Coffee: Diego Blas - Gravitational wave detection with orbita...
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Presentation in the Science Coffee of the Advanced Concepts Team of the European Space Agency on the 07.06.2024.
Speaker: Diego Blas (IFAE/ICREA)
Title: Gravitational wave detection with orbital motion of Moon and artificial
Abstract:
In this talk I will describe some recent ideas to find gravitational waves from supermassive black holes or of primordial origin by studying their secular effect on the orbital motion of the Moon or satellites that are laser ranged.Farming systems analysis: what have we learnt?.pptx
Presentation given at the official farewell of Prof Ken Gillet at Wageningen on 13 June 2024
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TOPIC OF DISCUSSION: CENTRIFUGATION SLIDESHARE.pptx
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The cost of acquiring information by natural selection
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The mangalyaan (after mission completion)
- 1. MARS ORBITER MISSION Submitted by: Akhilesh Rathiya Section - G Roll No. - 6 Submitted to: Mrs. Swarnita Sharma
- 2. •“The Mangalyaan” Mars Orbiter Mission (MOM) is a “Technological Demonstrator”. •It is India’s first interplanetary mission. •It was launched on 05th November 2013 by ISRO at Dhawan Space Center, Shriharikota. •The Total cost of mission was approximately 450 Crore INR, making it least expensive Mars Mission to date.
- 3. Mission Objectives Technical Objectives •Design and realization of Mars Orbiter. •Orbit around the Mars •Deep Space Communication, Navigation, Mission Planning and Management. Scientific Objectives •Exploration of Mars surface features. •Study of Morphology, Topography, Mineralogy and Martian atmosphere by Indigenous scientific instruments. •To see mars had the environment in which life evolved.
- 4. •Lyman-Alpha Photometer(LAP)– It is a Photometer that measures relative abundance of Deuterium and Hydrogen. •Methane Sensor for Mars(MSM) – It will measures methane in atmosphere of mars. •Mars Exospheric Neutral Composition Analyzer(MENCA) – Quadrupole Mass analyser capable of analsing the nuetral composition of particles in the exosphere. •Thermal Infrared Imaging Spectrometer (TIS) – It will measure the temperature and emissivity of the Martian surface. •Mars Colour Camera (MCC) – will provide images in the visual spectrum, providing context for the other instruments. Scientific Instruments
- 5. Scientists Behind The Mission 1. K Radhakrishnan: He is the Chairman of ISRO and Secretary in department of space. 2. M Annadurai: He is the Programme Director of Mars Orbiter Mission. 3. S Ramakrishnan: He is the Director of Vikram Sarabhai Space Centre and Member Launch Authorisation Board. 4. SK Shivakumar: He holds the position of the Director of ISRO Satellite Centre. 5. P Kunhikrishnan: The project director of PSLV programme. 6. Chandradathan: He is the Director of Liquid Propulsion system. 7. AS Kiran Kumar: The Director of Satellite Application Centre.
- 6. •8. MYS Prasad: The Director of Satish Dhawan Space Centre and Chairman of the Launch Authorisation Board. •9. S Arunan: The Project Director. •10. B Jayakumar: The Associate Project Director of PSLV project. •11. MS Pannirselvam: The Chief General Manager of range. •12. S Arunan: Project Director of Mars Orbiter Mission •13. V Kesava Raju: The Mission Director •14. ISRO scientific secretary V Koteswara Rao. Scientists Behind The Mission
- 7. The Grand Success Finally, After a long Period of 298 days on 24th September 2014 “The Mangalyaan” has arrived his destination and has captured it’s first photo. The successful entry of “Mangalyaan” into the Red Planet’s orbit is a once-in-generation achievement and “Indian Scientist Created History”, In “Never Before” moment. India has become fourth space agency to reach mars, in first attempt and first Asian nation to do so. With least expensive cost of about 450 crore INR. India has left China and Japan in race to explore the Red Planet. “The View is Nice up Here” #ISRO Official Tweet “We join the elite club of three other nation Russia, US and Europe and what is so special that we have success in the first attempt. -PM Modi