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  #1  
June 4th, 2016, 11:14 AM
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Mangalyan ISRO

Hello sir, I am Rohit. I want you to help me by giving me some information about the Mars Orbiter Mission (MOM) or Mangalyaan by Indian Space Research organization (ISRO). Can you help me?
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  #2  
June 4th, 2016, 12:38 PM
Super Moderator
 
Join Date: Mar 2012
Re: Mangalyan ISRO

As you have asked about the Mars Orbiter Mission (MOM) or Mangalyaan by Indian Space Research organization (ISRO), I am giving you information about it, check below for the details

It is space probe orbiting Mars since 24 September 2014.
It was launched on 5 November 2013 by the Indian Space Research Organisation (ISRO).
It is India's first interplanetary mission and ISRO has become the fourth space agency to reach Mars, after the Soviet space program, NASA, and the European Space Agency.

The mission is a "technology demonstrator" project to develop the technologies for designing, planning, management, and operations of an interplanetary mission.

The spacecraft is currently being monitored from the Spacecraft Control Centre at ISRO Telemetry, Tracking and Command Network (ISTRAC) in Bangalore with support from Indian Deep Space Network (IDSN) antennae at Byalalu.

Mission objectives

The primary objective of the Mars Orbiter Mission is to showcase India's rocket launch systems, spacecraft building and operations capabilities.

The secondary objective is to explore
Mars' surface features,
morphology,
mineralogy and Martian atmosphere using indigenous scientific instruments.

Spacecraft properties

Bus I-1K
Manufacturer ISAC
Launch mass 1,337 kg (2,948 lb)
BOL mass 550 kg (1,210 lb)
Dry mass 500 kg (1,100 lb)
Payload mass 15 kg (33 lb)
Dimensions 1.5 m (4.9 ft) cube
Power 840 watts
Start of mission
Launch date 5 November 2013, 09:08 UTC
Rocket PSLV-XL C25
Launch site Satish Dhawan FLP
Contractor ISRO
Orbital parameters
Reference system Areocentric
Periareon 421.7 km (262.0 mi)
Apoareon 76,993.6 km (47,841.6 mi)
Inclination 150.0°
Period 72 hours, 51 minutes, 51 seconds
Epoch Plannet
Mars orbiter
Orbital insertion 24 September 2014, 02:00 UTC
MSD 50027 06:27 AMT


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