PSLV-C35

PSLV-C35 was the successful mission of the

• Mass:
  • Total liftoff weight: 320,000 kilograms (710,000 lb)
  • Payload weight: 671.25 kilograms (1,479.9 lb)
• Overall height: 44.4 metres (145.7 ft)
• Propellant:
  • First stage:
    Solid HTPB based
    (138.2 + 6 x 8.9 tonnes)
  • Second stage:
    Liquid UH 25
    + N₂O₄ (42 tonnes)
  • Third stage:
    Solid HTPB based
    (7.6 tonnes)
  • Fourth stage:
    Liquid MMH + MON-3
    (2.5 tonnes)
• Engine:
  • First stage: Core (PS 1) + 6 strap-on PSOM
  • Second stage: Vikas
  • Third stage: PS 3
  • Fourth stage: PS 4
• Thrust:
  • First stage: 4,762 + 645 x 6 kN
  • Second stage: 800 kN
  • Third stage: 246 kN
  • Fourth stage: 7.3 x 2 kN
• Maximum altitude: 739.314 kilometres (459 mi)
• Maximum velocity:7,527.63 metres per second (24,697 ft/s) (recorded at time of PS-4 engine restart 2)
• Duration: 8,133 seconds

^[3]

Payload

PSLV-C35 carried and deployed eight satellites in two different

Country	Owner	Name	Nos	Mass	Type	Objective
India	ISRO	ScatSat-1	1	377 kg	Miniaturized satellite	Weather forecasting, cyclone prediction and tracking.
	IIT Bombay	Pratham	1	10 kg	Nanosatellite	Research satellite .
	PES Institute of Technology	PISat	1	5.25 kg		Remote sensing.[3][6]
Algeria	Agence Spatiale Algerienne	Alsat-1B	1	103 kg	Earth observation satellite	Agricultural and disaster monitoring.
		Alsat-2B	1	117 kg		Monitoring natural resources.
		Alsat-1N	1	7 kg	Cubesat	Technology demonstration satellite.[3][6]
Canada	UTIAS	CanX-7	1	8 kg
USA	Spaceflight Industries	Pathfinder-1	1	44 kg	micro-satellite	Earth imaging.[3][6]

See also

• Indian Space Research Organisation
• Polar Satellite Launch Vehicle