Nov 5, 2013

Mars Orbiter Mission Spacecraft

Mars Orbiter Mission is India's first interplanetary mission to planet Mars with an orbiter craft designed to orbit Mars in an elliptical orbit. The Mission is primarily technological mission considering the critical mission operations and stringent requirements on propulsion and other bus systems of spacecraft. It has been configured to carry out observation of physical features of mars and carry out limited study of Martian atmosphere with following five payloads:

  • Mars Colour Camera (MCC)
  • Thermal Infrared Imaging Spectrometer (TIS)
  • Methane Sensor for Mars (MSM)
  • Mars Exospheric Neutral Composition Analyser (MENCA)
  • Lyman Alpha Photometer (LAP)
Mars Orbiter Mission Spacecraft

Specifications

Lift-off Mass1337 kg
StructuresAluminium and Composite Fibre Reinforced Plastic (CFRP) sandwich construction-modified I-1 K Bus
MechanismSolar Panel Drive Mechanism (SPDM), Reflector & Solar panel deployment
PropulsionBi propellant system (MMH + N2O4) with additional safety and redundancy features for MOI. Proplellant mass:852 kg
Thermal SystemPassive thermal control system
Power SystemSingle Solar Array-1.8m X 1.4 m - 3 panels - 840 W Generation (in Martian orbit), Battery:36AH Li-ion
Attitude and Orbit Control SystemAOCE (Attitude and Orbit Control Electronics): with MAR31750 Processor; Sensors: Star sensor (2Nos), Solar Panel Sun Sensor (1No), Coarse Analogue Sun Sensor; Actuators: Reaction Wheels (4Nos), Thrusters (8Nos), 440N Liquid Engine
AntennaeLow Gain Antenna (LGA), Mid Gain Antenna (MGA) and High Gain Antenna (HGA)
Launch DateNov 05, 2013
Launch SiteSDSC SHAR Centre, Sriharikota, India
Launch VehiclePSLV - C25
MOM Payloads
MOM Payloads

About spacecraft

प्रमोचन भार / Launch Mass:1337 kg
शक्ति / Power:840 W
प्रमोचक राकेट / Launch Vehicle:PSLV-C25
उपग्रह का प्रकार / Type of Satellite:Science & Exploration
निर्माता / Manufacturer:ISRO
स्‍वामी / OwnerISRO
अनुप्रयोग / Application:Planetary Observation
कक्षा का प्रकार / Orbit Type:Martian

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