A Russian Soyuz-2-1b rocket suffered a rare pad abort during a launch attempt with the latest Resurs-P (No.3) remote sensing satellite for Roskosmos on Saturday. A realigned launch attempt took place on Sunday at Site 31/6 at the Baikonur Cosmodrome, with liftoff successfully occurring at 18:56 UTC.
Russian rockets are known for avoiding aborts and launching in most weather conditions. As such a pad abort with seconds remaining is very rare. It is believed this was the first pad abort for the Soyuz 2-1B.
While the Russians have suffered from failures, a pad abort during ignition – as is believed to be the case with this attempt, per a single line statement from Roscosmos – is very rare for any Russian vehicle.
Initially, no word was provided as to when the next attempt will take place. However, the launch window is only 10 seconds long, as such any hold or abort is an immediate scrub for the day. That may explain why the traditionally hardy Russian “pad rats” were seen running back to the vehicle just minutes after the abort was called.
Roscosmos later noted they will try again on Sunday, which proved to be without incident.
Part of Russia’s long-running Resurs program, Resurs-P No.3 is set to follow the previous two satellites, which has been in orbit since June 2013 and December 2014 respectively.
The 5,920-kilogram satellite is designed for five years of operational service, and is the second of five Resurs-P satellites planned. Resurs-P measures 7.93 metres in length and 2.72 metres in diameter at its widest point (26 by 8.9 feet).
Constructed by the TSSKB Progress design bureau, the satellite is based around a bus derived from the Yantar series of reconnaissance satellites.
The Yantar-derived bus has become a common element of Russian spacecraft in recent years, with many new-generation military satellites also based upon this platform.
The satellite is powered by twin solar arrays deployed from the aft end of the bus. These measure 5.0 by 4.5 metres (16.4 by 14.7 feet), producing electricity for Resurs-P No.3 and its instruments.
Roskosmos placed an order for the satellite in November 2010, with the satellite then expected for delivery in 2013 at a cost of 2.22 billion Roubles (43.5 million dollars).
The Resurs-P No.3 satellite carries an imaging payload consisting of high-resolution, hyperspectral and area survey instruments developed by TSSKB Progress and optical engineering company Krasnogorsky Zavod.
The satellite’s primary instrument is the Geoton-L1 panchromatic imager, which can image the surface at a resolution of 1.0 to 3.4 metres (3.3 to 11.2 feet). Images can be transmitted to the ground in real time, using the Sangur-1U downlink system.
Resurs-P No.3’s hyperspectral payload is designed to produce images at multiple wavelengths, with a spectral resolution of 5-10 nanometres. The 140 kilogram (310 lb) instrument can image the Earth’s surface with a resolution of up to 30 metres (98 feet).
The final part of the imaging payload consists of two multispectral cameras for area survey; one high-resolution and the other medium-resolution. In multispectral mode the cameras can produce images at resolutions of up to 119 kilometres and 23.8 kilometres (73.9 and 14.8 miles) respectively.
The cameras can also operate in a panchromatic mode, increasing their resolution to 11.9 and 59.4 kilometres (7.39 and 36.9 miles) respectively.
The multispectral imager operates at visible and near-infrared wavelengths, between 430 and 900 nanometres. Its high-resolution camera can image a 97.2 kilometre (60.4 mile) swath of the Earth’s surface, while the medium-resolution instrument has a swath width of 442 kilometres (275 miles).
Resurs-P No.3 also carries an AIS receiver, designed to collect and relay tracking and status data from ships at sea, to aid navigation and search and rescue operations.
Resurs was launched by Russia’s Soyuz-2-1b rocket. Derived from the older Soyuz-U and Soyuz-FG, the Soyuz-2 introduced modernised flight controls among other enhancements.
A three-stage rocket under Russian nomenclature, the Soyuz-2 consists of a core stage – termed the second stage – augmented by four liquid booster rockets which are termed the first stage.
The third stage sits atop the core. The Soyuz-2-1a and 2-1b variants differ in terms of the engine used to power the third stage – the Soyuz-2-1a uses the older RD-0110, while the Soyuz 2-1b makes use of the more capable RD-0124.
The smaller Soyuz-2-1v also uses the RD-0124-powered stage, however it omits the first stage and its core stage is re-engined with an NK-33.
The Soyuz-2 first flew in November 2004, making a suborbital test flight from the Plesetsk Cosmodrome. The type’s first orbital launch came almost two years later when EUMETSAT’s MetOp-A weather satellite was deployed by a Soyuz-2-1a/Fregat flying from Baikonur.
The Soyuz-2-1b made its maiden flight later that year, deploying the CoRoT observatory for CNES and the European Space Agency.
Soyuz-2 launches from the Baikonur Cosmodrome make use of Site 31/6, one of two pads at the facility used by Soyuz and formerly other R-7-derived rockets – the other pad being Site 1/5.
First built for test launches of the R-7A missile, Site 31 was first used for an orbital launch in November 1962, by an R-7 flying in the obscure 11A59 configuration – known in various sources as Sputnik or Polyot – to orbit a prototype antisatellite weapon.
Site 31/6 is currently the only pad at Baikonur which can support the Soyuz-2, with 1/5 expected to be refitted in the near future.
Older versions still flying, such as the Soyuz-U which carries Progress resupply missions to the International Space Station and the Soyuz-FG which is mostly used for manned launches of the Soyuz-TMA spacecraft, can use either pad and from time to time Site 31 is even used for manned launches.
Soyuz rockets are integrated horizontally away from the launch pad. Ahead of liftoff, the Soyuz rocket was transported to Site 31 by train and erected on the launch pad.
About seventeen seconds before liftoff, the first and second stage engines ignited. The Soyuz-2’s first stage is powered by four RD-107A engines, while a single RD-108A is powered the second stage.
These engines build up to full thrust through the final seconds of the countdown, while at the zero mark four swing arms retracted from the base of the vehicle freeing it to ascend to orbit.
The first stage burns for around 117 seconds before burnout and separation from the core vehicle. Second stage flight continues for a further 170 seconds, with third stage ignition and separation occurring four minutes and 47 seconds into the flight.
A second after ignition, interstage panels protecting the third stage engine bay during ascent are jettisoned, with the payload fairing separating from the nose of the vehicle at around the same time.
The third stage’s RD-0124 engine burns for four minutes and 33 seconds, completing the injection of Resurs-P No.2 into its initial deployment orbit.
The target orbit for the launch is a perigee of 200 kilometres (124 miles or 108 nautical miles), an apogee of 475 kilometres (295 miles, 256 nautical miles) and inclination of 97.285 degrees.
The spacecraft will circularise this trajectory at apogee during the first few days of its mission, putting itself into an operational sun-synchronous orbit.
(Images via Roscosmos)