UK-DMC3A/B/C & Rideshares

Launch Success

Liftoff Time (GMT)

16:28:00

Friday July 10, 2015

Mission Details

Launch Notes

At the time it was the heaviest commercial mission (1439 kg) successfully accomplished using a launch vehicle assembled by ISRO.

UK-DMC3A

Wiki

UK-DMC 3 is a constellation of three British Earth-imaging satellites which are operated by DMC International Imaging. They were constructed by Surrey Satellite Technology

Sun-Synchronous Orbit

1 Payload

440 kilograms

UK-DMC3B

Wiki

UK-DMC 3 is a constellation of three British Earth-imaging satellites which are operated by DMC International Imaging. They were constructed by Surrey Satellite Technology

Sun-Synchronous Orbit

1 Payload

440 kilograms

UK-DMC3C

Wiki

UK-DMC 3 is a constellation of three British Earth-imaging satellites which are operated by DMC International Imaging. They were constructed by Surrey Satellite Technology

Sun-Synchronous Orbit

1 Payload

440 kilograms

Carbonite 1

Wiki

Carbonite 1 or CBNT 1 is a microsatellite for technology demostrations built by SSTL. The mission is to test some technical EO capabilities, new process and rapid-build techniques. Carbonite uses a commercial off-the-shelf camera and 0.25 m telescope to acquire videos and still pictures of Earth. Both modes show features on the ground down to a size of 1.5 m. The telescope can be disassembled and integrated into a new specially designed framework in 5 days.

Sun-Synchronous Orbit

1 Payload

91 kilograms

DeOrbitSail

Wiki

The DeOrbitSail is a project to build a 3U CubeSat sized satellite with a deployable sail that will demonstrate rapid deorbiting. The DeOrbitSail project is a cooperation between Surrey Space Centre (UK), Caltech (USA), DLR (Germany), EADS Astrium (France), Stellenbosch University (South Africa), University of Patras (Greece), Athena-SPU (Greece), Middle-Eastern Technical University (Turkey), Surrey Satellite Technology Limited (SSTL) (UK), ISIS (Netherlands). The deorbiting capability of the DeOrbitSail satellite is due to increased aerodynamic drag from the large surface area of the deployed sail in a Low Earth Orbit (LEO).

Sun-Synchronous Orbit

1 Payload

7 kilograms

Rocket

Active
PSLV-XL

Active Since 2008

Indian Space Research Organisation logo

Agency

ISRO

Price

$31.00 million

Rocket

Height: 44m

Payload to Orbit

LEO: 3,250 kg

GTO: 1,410 kg

Liftoff Thrust

7,661 Kilonewtons

Fairing

Diameter: 3.2m

Height: 8.3m

Stages

4

Strap-ons

6

Launch Site

First Launch Pad

Satish Dhawan Space Centre, India

Fastest Turnaround

25 days 5 hours

Stats

PSLV


30th

Mission

2nd

Mission of 2015

Indian Space Research Organisation


47th

Mission

2nd

Mission of 2015

2015


35th

Orbital launch attempt