OrbitalHub

NASA dicit:

NASA’s Starling mission is advancing the readiness of various technologies for cooperative groups of spacecraft – also known as distributed missions, clusters, or swarms. Starling will demonstrate technologies to enable multipoint science data collection by several small spacecraft flying in swarms. The six-month mission will use four CubeSats in low-Earth orbit to test four technologies that let spacecraft operate in a synchronized manner without resources from the ground. The technologies will advance the following capabilities: swarm maneuver planning and execution, communications networking, relative navigation, autonomous coordination between spacecraft.

The Starling mission will test whether the technologies work as expected, what their limitations are, and what developments are still needed for CubeSat swarms to be successful.

Distributed spacecraft are advantageous because they can act in unison to achieve objectives. Incorporating autonomy allows these missions to act cooperatively with minimal oversight from the ground. Autonomy ensures that a mission continues to perform through periods when communications with a spacecraft from the ground is temporarily unavailable because of distance or location. Spacecraft swarms operating at great distances from the Earth must act more autonomously due to the delays in time communicating with Earth ground stations.

Clustering satellites into a swarm requires planning and executing multiple maneuvers for each spacecraft. Managing these operations from the ground becomes impractical as the size of the swarm grows or the time delay in communicating with the spacecraft increases. The Starling mission will test technologies that traditionally run ground-oriented operations but are now shifted to operate onboard the spacecraft.

Having the spacecraft in a swarm operate autonomously is essential to making distributed spacecraft missions affordable and highly scaleable. Starling is a first step in developing this new mission architecture that could eventually allow for autonomous swarms of many spacecraft and at greater distances from Earth.

The four 6-unit CubeSats (each about the size of two stacked cereal boxes) will fly in a Sun-synchronous orbit more than 300 miles above Earth and no more than 170 miles apart from each other. The spacecraft will fly in two formations. First, they will begin in line, or in-train, like a string of pearls. Then, the CubeSats will move out of the in-train configuration and into a set of stable relative orbits known as passive safety ellipses.

The following four technologies will be tested:

Reconfiguration and Orbit Maintenance Experiments Onboard (ROMEO): In each phase, cluster flight control software will initially operate in shadow mode, autonomously planning maneuvers while the CubeSats are controlled from the ground. Once validated, ROMEO will demonstrate execution of swarm maintenance maneuvers from aboard the spacecraft without ground intervention. The performance of those maneuvers will then be evaluated.

Mobile Ad-hoc Network (MANET): The CubeSats will be able to communicate with each other via two-way S-band crosslink radios/antennas, adapting a ground-based network protocol for reliable space communication across any spacecraft node within the swarm. If one spacecraft communications node fails, the communications route automatically reconfigures to maintain full communication capabilities for the remaining operational swarm of spacecraft.

Starling Formation-Flying Optical Experiment (StarFOX): Using commercial star trackers, which are onboard cameras that measure the position of stars, each spacecraft determines its own orientation relative to the stars. An advanced navigation algorithm utilizes this orientation data and star tracker images to visually detect and track the other three spacecraft within the swarm to perform relative-position knowledge tests. The goal is for each spacecraft to achieve onboard awareness of its location as well as the location of the other three spacecraft.

Distributed Spacecraft Autonomy (DSA): This experiment will demonstrate autonomous monitoring of Earth’s ionosphere, the layer between our atmosphere and the beginning of space, with a spacecraft swarm. This is intended as a representative measurement to demonstrate autonomous reactive operations for future missions. Starling’s dual-band GPS receivers are used to measure the density of atmospheric regions. Each orbiting Starling spacecraft constantly changes position relative to the atmospheric phenomenon and the GPS satellites. Therefore, the most interesting source of information changes over time, requiring changes to the monitoring strategy in response to observations. DSA onboard software will autonomously coordinate the selection of the best GPS signals, across all Starling spacecraft, to accurately capture regions of higher or lower ionospheric density. This is accomplished by first sharing information over the crosslink network to maintain a consistent state, then selecting the GPS signals to prioritize and share in the future. The ability to evaluate data as it is collected, balance promising observations with coverage to ensure other interesting information is not missed, and autonomously coordinate measurements, is an enabling technology for future science missions.

It’s important to note that although Starling is being tested in low-Earth orbit, the technologies apply equally as well to deep space applications. In the future, constellation-like swarms of autonomously operating CubeSats could provide NASA and commercial missions in deep space with navigation services akin to GPS and communications relays provided by Earth’s network of communications satellites. Distributed spacecraft can also work together to collect multi-point science data and prepare for exploration missions by positioning multiple small spacecraft to function as one very large observation instrument. This could support the identification of resources for long-term presence on the Moon. Another example of this cooperative work might include telescopes mounted on multiple small spacecraft and trained on a particular observation target, creating a larger field of view than possible with a single telescope.

Video credit: NASA’s Ames Research Center

Wikipedia dicit:

A rotating detonation engine (RDE) is an engine using a form of pressure gain combustion, where one or more detonations continuously travel around an annular channel. Computational simulations and experimental results have shown that the RDE has potential in transport and other applications.

In detonative combustion, the results expand at supersonic speed. It is theoretically more efficient than conventional deflagrative combustion by as much as 25%. Such an efficiency gain would provide major fuel savings. Disadvantages include instability and noise.

The basic concept of an RDE is a detonation wave that travels around a circular channel (annulus). Fuel and oxidizer are injected into the channel, normally through small holes or slits. A detonation is initiated in the fuel/oxidizer mixture by some form of igniter. After the engine is started, the detonations are self-sustaining. One detonation ignites the fuel/oxidizer mixture, which releases the energy necessary to sustain the detonation. The combustion products expand out of the channel and are pushed out of the channel by the incoming fuel and oxidizer.

Although the RDE’s design is similar to the pulse detonation engine (PDE), the RDE is superior because the waves cycle around the chamber, while the PDE requires the chambers to be purged after each pulse.

Credit: NASA’s Marshall Space Flight Center

Wikipedia dicit:

A launch escape system (LES) or launch abort system (LAS) is a crew-safety system connected to a space capsule that can be used to quickly separate the capsule from its launch vehicle in case of an emergency requiring the abort of the launch, such as an impending explosion. The LES is typically controlled by a combination of automatic rocket failure detection, and a manual activation for the crew commander’s use. The LES may be used while the launch vehicle is still on the launch pad, or during its ascent. Such systems are usually of two types: solid-fuelled rocket or ejection seats.

A solid-fuelled rocket, mounted above the capsule on a tower, which delivers a relatively large thrust for a brief period of time to send the capsule a safe distance away from the launch vehicle, at which point the capsule’s parachute recovery system can be used for a safe landing on ground or water. The tower and rocket are jettisoned from the space vehicle in a normal flight at the point where it is either no longer needed, or cannot be effectively used to abort the flight. These have been used on the Mercury, Apollo, Soyuz, and Shenzhou capsules.

The crew are seated in seats that eject themselves (ejection seats) as used in military aircraft; each crew member returns to Earth with an individual parachute. Such systems are effective only in a limited range of altitudes and speeds. These have been used on the Vostok and Gemini capsules.

Credit: NASA’s Ames Research Center

Wikipedia dicit:

The Surface Water and Ocean Topography (SWOT) mission is a satellite altimeter jointly developed and operated by NASA and CNES, the French space agency, in partnership with the Canadian Space Agency (CSA) and UK Space Agency (UKSA). The objectives of the mission are to make the first global survey of the Earth’s surface water, to observe the fine details of the ocean surface topography, and to measure how terrestrial surface water bodies change over time.

While past satellite missions like the Jason series altimeters (TOPEX/Poseidon, Jason-1, Jason-2, Jason-3) have provided variation in river and lake water surface elevations at select locations, SWOT will provide the first truly global observations of changing water levels, stream slopes, and inundation extents in rivers, lakes, and floodplains. In the world’s oceans, SWOT will observe ocean circulation at unprecedented scales of 15–25 km (9.3–15.5 mi), approximately an order of magnitude finer than current satellites. Because it uses wide-swath altimetry technology, SWOT will almost completely observe the world’s oceans and freshwater bodies with repeated high-resolution elevation measurements, allowing observations of variations.

Credit: NASA/JPL-Caltech/CNES

NASA JPL dicit:

NASA and the European Space Agency are developing plans for one of the most ambitious campaigns ever attempted in space: bringing the first samples of Mars material safely back to Earth for detailed study. The diverse set of scientifically curated samples now being collected by NASA’s Mars Perseverance rover could help scientists answer the question of whether ancient life ever arose on the Red Planet.

Bringing samples of Mars to Earth for future study would happen in several steps with multiple spacecraft, and in some ways, in a synchronized manner. This short animation features key moments of the Mars Sample Return campaign: from landing on Mars and securing the sample tubes to launching them off the surface and ferrying them back to Earth.

Credit: NASA/ESA/JPL-Caltech/GSFC/MSFC

NASA dicit:

NASA’s Low-Earth Orbit Flight Test of an Inflatable Decelerator (LOFTID) is currently at Vandenberg Space Force Base in California, where teams are preparing the novel technology for launch as a secondary payload with the National Oceanic and Atmospheric Administration’s (NOAA) Joint Polar Satellite System-2 (JPSS-2) satellite, which will help track and predict Earth’s weather and climate.

Credit: NASA Langley Research Center