PSLV-C55
{{Short description|Indian satellite launch mission}}
{{Multiple issues|
{{More footnotes needed|date=April 2023}}
{{One source|date=April 2023}}
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{{Infobox rocket launch
|name = PSLV-C55
|image=PSLV-C55, TeLEOS-2 - Launch vehicle lifting off from First Launch Pad (FLP) of SDSC-SHAR 03.webp
|caption=PSLV - C55 lifts off on First Launch Pad
|launch = 22 April 2023
08:49 (UTC)
|pad = First Launch Pad Satish Dhawan Space Centre
|payload = {{flagicon|Singapore}} TeLEOS-2
{{flagicon|Singapore}} Lumelite-4
{{flagicon|India}}
7× smaller payloads hosted on POEM-2 (PSLV Orbital Experimental Module-2)
|succession = PSLV launches
|previous = PSLV-C54
|next = PSLV-C56 }}
The PSLV-C55 was the 57th mission of Indian Space Research Organisation's Polar Satellite Launch Vehicle (PSLV) and the 16th flight of the PSLV-CA variant.PSLV-C55/TeLEOS-2 Mission Brochure [https://www.isro.gov.in/media_isro/pdf/Missions/PSLVC55/PSLVC55TeLEOS.pdf#page=2 https://www.isro.gov.in/media_isro/pdf/Missions/PSLVC55/PSLVC55TeLEOS.pdf]
Launch
It was launched on Saturday, 22 April 2023 at 14:19 IST / 08:49 UTC from Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh, India.{{Cite news |last=Kandavel |first=Sangeetha |date=2023-04-22 |title=ISRO PSLV-C55 successfully launches two Singapore satellites into orbit |language=en-IN |work=The Hindu |url=https://www.thehindu.com/sci-tech/science/isro-successfully-launches-pslv-c55-mission-carrying-two-singaporean-satellites/article66766469.ece |access-date=2023-04-22 |issn=0971-751X}}{{Cite web |title=ISRO's PSLV-C55 lifts off with two Singaporean satellites, 7 Indian 'experiments' in textbook launch |url=https://www.indiatoday.in/science/story/isros-pslv-c55-launch-singapore-satellite-poem-space-mission-2363298-2023-04-22 |access-date=2023-08-24 |website=India Today |language=en}} This was a dedicated commercial mission through NSIL with TeLEOS-2 as primary satellite and Lumelite-4 as a co-passenger satellite weighing 741 kg and 16 kg respectively. Both satellites belong to Singapore.{{Cite web |date=2023-04-22 |title=PSLV C55 Launch Live Updates: Isro's PSLV-C55 successfully places two Singapore satellites into orbit |url=https://timesofindia.indiatimes.com/india/pslv-c55-launch-live-updates-isro-to-launch-two-singaporean-satellites-teleos-2-lumelite-4-from-sriharikot/liveblog/99685441.cms |access-date=2023-08-24 |website=The Times of India |language=en}}
Mission overview
Primary payload: TeLEOS-2
Secondary payload: Lumelite-4
This also marks the third time that PS4 is used after satellite separations as a platform for experiments. There are non-separable payloads mounted on MSA (multi-satellite adapter).{{Cite news |author= |date=2023-04-20 |title=PSLV-C55 mission: How ISRO will use spent PS4 |language=en-IN |work=The Hindu |url=https://www.thehindu.com/sci-tech/science/pslv-c55-mission-isro-to-carry-out-in-orbit-scientific-experiments-using-spent-ps4/article66758527.ece |access-date=2023-08-24 |issn=0971-751X}} Payloads are powered on by a command after all satellites are separated. The orbital platform will remain in the same orbit achieved at the end of PS4 tank passivation after the primary mission. It has an expected life of 1 month.
As a part of POEM-2 (PSLV Orbital Experimental Module), there are seven experimental non-separable payloads:{{Cite web |last=Graham |first=William |date=2023-04-22 |title=ISRO launches PSLV with Singaporean satellites |url=https://www.nasaspaceflight.com/2023/04/isro-to-launch-pslv-with-singaporean-satellites/ |access-date=2023-08-24 |website=NASASpaceFlight.com |language=en-US}}
- PiLOT (PSLV In orbitaL Obc and Thermals) OBC package from IIST
- OBC package from IIST
- ARIS-2 (Advanced Retarding Potential analyser for Ionospheric Studies) experiment from IIST
- HET based ARKA200 Electric Propulsion System from Bellatrix Aerospace
- DSOD-3U and DSOD-6U deployer units along with DSOL-Transceiver in S- & X- bands from Dhruva Space
- Starberry Sense Payload from Indian Institute of Astrophysics (IAP)
| class="wikitable"
!Parameter !Orbit-1 |
| Semi-Major Axis (km)
|6964 |
| Alt (km)
|586 |
| Eccentricity
|0.0 |
| Inclination (deg.)
|10.00 |
| Launch Pad
|FLP |
| Launch Azimuth (deg.)
|104 |
- Stage 1: Composite Solid (HTBP based)
- Stage 2: Earth Storable Liquid (UDMH + N2O4)
- Stage 3: Composite Solid (HTBP based)
- Stage 4: Earth Storable Liquid (MMH + MON3)
The PSLV C55 rocket has four stages; each one was self-contained, with its own propulsion system, thereby capable of functioning independently. The first and third stages used composite solid propellants, while the second and fourth stage use earth-storable liquid propellant.
References
{{reflist}}
{{Cite web | last=Surendra | first=Singh | date=2023-04-13 | title = With PSLV-C55 mission, Isro uses new rocket Integration|url= https://timesofindia.indiatimes.com/india/with-pslv-c55-mission-isro-uses-new-rocket-integration-technique-to-cut-time/articleshow/99446716.cms|access-date=2023-04-13 |website=Timesofindia |language=en}}
{{Cite web | last=Satish Dhawan| first=Space Centre| date=2023-04-17 | title = Registration for Launch View Gallery, PSLV-C55 Mission|url= https://lvg.shar.gov.in/VSCREGISTRATION/index.jsp |access-date=2023-04-17 |website=Satish dhawan space centre|language=en}}
{{PSLV}}
Category:Polar Satellite Launch Vehicle