PSLV-DL variant has only two strapons boosters with 12 tonne propellant load on them. PSLV-C44 on 24 January 2019 was the first flight to use PSLV-DL variant of Polar Satellite Launch Vehicle.
Specifications
- Thrust
- —
- Height
- 44 m
- Diameter
- 2.8 m
- Launch mass
- —
- Stages
- 4
- Launch cost
- —
- LEO capacity
- 3,800 kg
- GTO capacity
- 1,200 kg
- GEO capacity
- —
- SSO capacity
- 1,750 kg
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
5
Launches with a definitive outcome
Success rate
80%
4 of 5
Current success streak
0
Landings
0
0 attempts · 0 droneship / 0 RTLS
Fastest turnaround
—
Between consecutive booster flights
Counted from padside's own launch record — the same basis as the Stats page.
Launches
- PSLV-DL | EOS-N1 and others — Failure
- PSLV-DL | XPoSat — Success
- PSLV-DL | Amazonia 1 & 18 others — Success
- PSLV-DL | EOS-01 (RISAT-2BR2) — Success
- PSLV-DL | Microsat-R — Success