Oval orbit casts new light on black hole, neutron star mergers

Scientists have uncovered the first robust evidence of a black hole and neutron star crashing together but orbiting in an oval path rather than a perfect circle just before they merged. This discovery challenges long-standing assumptions about how these cosmic pairs form and evolve.

Researchers from the University of Birmingham, Universidad Autónoma de Madrid, and Max Planck Institute for Gravitational Physics published their findings today (11 Mar) in The Astrophysical Journal Letters.

Most neutron star-black hole pairs are expected to adopt circular orbits long before merging. But the analysis of the gravitational-wave event GW200105 shows that this system travelled on an oval orbit long before merging to form a black hole 13 times more massive than the Sun. An oval orbit is something never seen before in this kind of collision.

Dr Patricia Schmidt, from the University of Birmingham, said: “This discovery gives us vital new clues about how these extreme objects come together. It tells us that our theoretical models are incomplete and raises fresh questions about where in the Universe such systems are born.”

The researchers analysed data from LIGO and Virgo detectors using a new gravitational‑wave model developed at the University of Birmingham’s Institute of Gravitational Wave Astronomy. This allowed them to measure both how ‘oval’ the orbit was (eccentricity) and any spin‑induced wobbling (precession). This is the first time these two effects have been measured together in a neutron star–black hole event.

Geraint Pratten, a Royal Society University Research Fellow from the University of Birmingham, said: “The orbit gives the game away. Its elliptical shape just before merger shows this system did not evolve quietly in isolation but was almost certainly shaped by gravitational interactions with other stars, or perhaps a third companion.”

A Bayesian analysis comparing thousands of theoretical predictions to the real data, showed that a circular orbit is extremely unlikely, ruling it out with 99.5% confidence.

Past analyses of GW200105, which assumed a circular orbit, underestimated the black hole mass and overestimated the neutron star mass. The new study corrects these values and finds no compelling evidence of precession, indicating that the eccentricity was imprinted by its formation rather than by spins.

Gonzalo Morras, from the Universidad Autónoma de Madrid and the Max Planck Institute for Gravitational Physics, said: “This is convincing proof that not all neutron star–black hole pairs share the same origin. The eccentric orbit suggests a birthplace in an environment where many stars interact gravitationally.”

This discovery challenges the prevailing view that all neutron star–black hole mergers arise from a single dominant formation channel and highlights the need for more advanced waveform models capable of capturing the full complexity of these systems.

The study helps to explain the growing diversity seen in compact-binary mergers and opens the door to identifying even more unusual pathways as the number of gravitational-wave detections continues to grow.

Chandrayaan-II update: Orbiter completes thermo-vacuum test

Chandrayaan-2, India’s second mission to the Moon, is a totally indigenous mission comprising of an Orbiter, Lander and Rover. It envisages complex tasks like soft-landing, Rover separation and movement on the lunar surface, in addition to operations of Orbiter, informed Minister Jitendra Singh in a written reply to a question in the Lok Sabha on Monday.

Several new technology elements have been developed indigenously and tests are being carried out for validation. Orbiter has completed Thermo-vacuum test which is one of the major milestones, he said.

Lander Sensors and Actuators are tested on ground to validate the performance and the results are satisfactory, while rover flight model is under assembly, said the minister. Payloads are in various stages of delivery for Spacecraft integration, he informed the House.

After reaching the 100 km lunar orbit, the Lander housing the Rover will separate from the Orbiter. After a controlled descent, the Lander will soft land on the lunar surface at a specified site and deploy a Rover, said Indian Space Research Organisation (ISRO).

The mission will carry a six-wheeled Rover which will move around the landing site in semi-autonomous mode as decided by the ground commands. The instruments on the rover will observe the lunar surface and send back data, which will be useful for analysis of the lunar soil.

The Chandrayaan-2 weighing around 3290 kg and would orbit around the moon and perform the objectives of remote sensing the moon. The payloads will collect scientific information on lunar topography, mineralogy, elemental abundance, lunar exosphere and signatures of hydroxyl and water-ice.

To be carried by GSLV-F10, Chandrayaan-2 Mission is planned during first half of 2018.

ISRO Launches GSLV Mk III Successfully with GSAT-19 Satellite

The first developmental flight (GSLV MkIII-D1) of India’s heavy lift launch vehicle GSLV Mk-III was successfully conducted today (June 05, 2017) evening from Satish Dhawan Space Centre SHAR, Sriharikota with the launch of GSAT-19 satellite.
This was the first orbital mission of GSLV MkIII which was mainly intended to evaluate the vehicle performance including that of its fully indigenous cryogenic upper stage during the flight. Weighing 3136 kg at lift-off, GSAT-19 is the heaviest satellite launched from the Indian soil.

After a twenty five and a half hour smooth countdown, the mission began with the launch of the 640 ton GSLV Mk-III at 5:28 pm IST from the Second Launch Pad as scheduled with the ignition of its two S200 solid strap-on boosters. Following this, the major phases of the flight occurred as scheduled. The upper stage of GSLV MkIII vehicle is a new cryogenic stage (C25) indigenously configured, designed and realised by ISRO.

The cryogenic stage used liquid Hydrogen and liquid Oxygen as propellants with a total loading of 28 tons. The stage is powered by a 20 ton thrust cryogenic engine (CE20) operating on “gas generator cycle”. The performance of the engine and stage during the mission was as predicted. About sixteen minutes after lift-off, GSAT-19 satellite was successfully placed in orbit.

Soon after its separation from GSLV, the Master Control Facility (MCF) at Hassan in Karnataka assumed control of the satellite. GSAT-19 is a high throughput communication satellite.

In the coming days, GSAT-19 orbit will be raised from its present Geosynchronous Transfer Orbit (GTO) to the final circular Geostationary Orbit (GSO) by firing the satellite’s Liquid Apogee Motor (LAM) in stages. During the final phase of this operation, the solar panels and antenna reflectors of the satellite will be deployed. The satellite will be commissioned into service after its positioning in the designated slot in the GSO following in-orbit testing of its payloads.