Showing posts with label 背景知識. Show all posts
Showing posts with label 背景知識. Show all posts

Monday, March 3, 2025

Orbits of the Heart: The Science Behind "Star Rider"


Solar System Fundamentals


The Solar System, our home star system, was formed approximately 4.6 billion years ago from the gravitational collapse of a nebula. Over 99% of its mass eventually concentrated in the Sun, our central star. The remaining material, through the system’s evolutionary processes, gradually formed the eight planets and planetary belts, which serve as the primary destinations for interstellar exploration in my sci-fi novel “Star Rider”.

At the core of the Sun, due to the immense gravitational forces generated by its massive mass, a process of nuclear fusion occurs where vast quantities of protons (hydrogen nuclei) fuse into helium nuclei, releasing high-energy X-rays and gamma rays. These high-energy photons, originating from the Sun’s core, take thousands to as long as 50 million years to reach the Sun’s surface. During this journey, they are gradually converted into visible light and lower-energy radiation before escaping into space. In essence, the entire Solar System’s energy originates from the Sun’s nuclear fusion process.

This brings us to the concept of the “nuclear fusion engine,” which is repeatedly mentioned in the novel. Such an engine operates using technology similar to that of the Sun’s nuclear fusion. This technological level serves as the foundation of the novel’s world. By this era, humanity has begun extensive exploration within the Solar System, constructing numerous satellite cities to harness and utilize energy resources.
Planetary Distances and Planetary Belts

How far are Jupiter and Saturn? Where is the asteroid belt? What about the Kuiper Belt? Why do Ami and Alcon’s missions take years? Let’s break it down.
 

Solar System Scale




A distance scale diagram illustrates the structure of the Solar System. On this diagram, the leftmost section represents the Sun’s surface. The horizontal axis proportionally displays the distances of the planets from the Sun (though the planet sizes are not to scale). You’ll notice that Mercury, Venus, Earth, and Mars are clustered close together on the left side, marked by red vertical lines. Beyond Mars lies the asteroid belt, which serves as a natural boundary dividing the Solar System into two regions:

  • The Inner Solar System: Composed of rocky planets, including Earth, which is the third terrestrial planet from the Sun.
  • The Outer Solar System: Beyond the asteroid belt, containing the gas giants—Jupiter, Saturn, Uranus, and Neptune.
  • The red X-axis on the diagram includes two unit markers:
  • 1.5 E8 km – 150 million kilometers, the standard Earth-Sun distance in kilometers.
  • AU (Astronomical Unit) – One AU equals the Earth-Sun distance (150 million km).


With this unit in mind, we can estimate distances:

  • The asteroid belt is relatively close, making it an ideal first exploration ground for DSF astronauts.
  • Jupiter is about 5 AU from the Sun.
  • Saturn is about 10 AU from the Sun—10 times the Earth-Sun distance.
  • Uranus lies at 20 AU and Neptune at 30 AU.
  • Beyond Neptune, at 33 AU, lies the beginning of the Kuiper Belt.


In the novel, Alcon’s DSF3137, equipped with a powerful Category KU-2 engine, travels across space at a safe speed, taking approximately 9 Earth days per AU. Even if traveling in a straight line with no course adjustments, reaching Neptune’s orbit (without even entering the Kuiper Belt) already requires nearly 300 days. This immense scale of time and distance plays a critical role in shaping the narrative of Star Rider.
 

Planetary Size Comparison


The previous distance diagram was not to scale in terms of planet sizes. A separate diagram illustrating true planetary proportions highlights the vast differences:



The tiny rocky planets—Mercury, Venus, Earth, and Mars—are minuscule compared to the gas giants.

Earth appears strikingly small in contrast to the behemoths like Jupiter and Saturn.

In the novel, Earth is sometimes referred to as the “home planet”. This tiny blue sphere in the vastness of space remains humanity’s cradle.

Asteroids Mining


In the novel, humanity has constructed numerous space cities primarily between Earth and Mars. This region offers an optimal solar distance for habitation but lacks abundant building materials. As a result, the nearby asteroid belt serves as a crucial resource hub for constructing space infrastructure. While the outer Solar System contains massive planets, they are gas giants and unsuitable for human settlement. However, many space cities have also been built on the rocky moons of these gas giants, despite the potential risks posed by asteroid and comet impacts.

According to human technological advancements, metal materials, with their excellent ductility and malleability, are the best engineering materials. So, can such metal materials be obtained from the asteroid belt? --- The answer is: Yes. Instead not all asteroids are suitable for resource extraction. Based on spectral analysis, asteroids fall into three primary categories:

  • C-type (Carbonaceous) asteroids – 75% of known asteroids, primarily composed of carbon compounds.
  • S-type (Silicaceous) asteroids – 17% of known asteroids, containing iron, magnesium, and silicon.
  • M-type (Metallic) asteroids – Around 8% of the total number of asteroids in the asteroid belt, contain nickel and iron, believed to be remnants of planetary cores.


In Star Rider, C-type and S-type asteroid mining is still under research, while M-type asteroids are the primary targets for mining. Ami and Alcon, as exploration pilots, search for these asteroids, marking them with tracking beacons. Once identified, they become company assets, with tug ships towing them to designated mining locations for extraction and processing.

Beyond Neptune, the Kuiper Belt contains numerous celestial bodies, including Pluto, which was demoted to a dwarf planet. Due to its vast distance and high exploration costs, Kuiper Belt expeditions are more akin to territorial claims than profitable ventures. In Star Rider, Alcon is among the first explorers to enter this region, earning the title KU-2 certified pilot.


Lagrange Points


First, an important concept in celestial mechanics is the "Lagrange point." According to Wikipedia, a Lagrange point (also known as a libration point) is one of the five particular solutions to the restricted three-body problem in celestial mechanics.

Simply put, when two massive celestial bodies are in orbital motion, five equilibrium points emerge where smaller celestial bodies can achieve dynamic equilibrium. Many explanations refer to this as a "three-body" solution, but that is not entirely accurate. In the three-body problem, the three masses are usually of similar scale, whereas in the concept of Lagrange points, the focus is on "two massive celestial bodies and one or more much smaller bodies that do not significantly affect the gravitational environment.".

The simplified diagram of Lagrange points looks as follows: within the gravitational and dynamic environment created by two massive celestial bodies, five libration points labeled. These are commonly referred to as L1, L2, L3, L4, and L5. A small celestial body at any of these points can remain relatively "stable" or orbit around the corresponding equilibrium point.







Looking at our solar system, the Sun accounts for 99.86% of the system’s mass, and Jupiter alone is 2.5 times the combined mass of all other planets (see the planetary mass table below, sourced from NASA). We can apply the concept of Lagrange points to explain the motion of asteroids within the Asteroid Belt.


we used a top-down view of the ecliptic plane showing the asteroid belt. If we simplify that diagram, we get the following:



The white ring between Mars and Jupiter represents the Main Asteroid Belt. This asteroid belt is relatively close to the home planet - Earth, just beyond Mars’ orbit (though still over 2 AU away). This is the initial training ground for DSF pilots. However, looking slightly further out along Jupiter’s orbit (Jupiter is marked in the lower-right of the diagram), we find two additional groups of small celestial bodies labeled "Trojan Asteroids." Wait—why are they using Jupiter’s orbit?

These are the Trojan asteroid groups, which share Jupiter’s orbit and reside at L4 and L5. The L4 group was initially called the "The Greek asteroids" , though early naming conventions were inconsistent. As more Trojan asteroids were discovered, a structured naming system emerged, but some naming errors persisted. As a result, some Greek heroes' names appear among the Trojans, and vice versa. Regardless, these groups are located at the Sun-Jupiter L4/L5 Lagrange points, co-orbiting with Jupiter.




--- Start of Quote ---
Alcon's Journal # 12
Finally, after leaving the asteroid belt, we will need to perform one last major maneuver to adjust our trajectory to a relatively sparse and safe departure zone. This safe departure zone must allow us to take advantage of the gravitational pull of other planets on our future trajectory, while avoiding the Hilda and Trojan asteroid groups that are located at the Sun-Jupiter Lagrange points.

Mars evaluated the situation and confirmed that we have enough propellant to perform all of these maneuvers. Although Jupiter is not in our path this time, we will still need to avoid the Trojan asteroid group that shares Jupiter's orbit. By the time we reach Jupiter, the Galileo space habitat and the supply station on Amalthea(3th moon of Jupiter) will be quite far away, and there will be a lot of small celestial bodies blocking our view or hiding behind Jupiter, so we may not be able to see it clearly.
--- End Quote ---





Asteroid Belt Structure and Orbital Mechanics


During Alcon’s first Kuiper Belt expedition, he needed a safe route through the asteroid belt. Mars calculated a trajectory to avoid dense asteroid clusters. This brings us to another asteroid group—the Hilda asteroids. What are these?

Looking again at the more detailed ecliptic plane map from the previous chapter, you are now familiar with the white main asteroid belt and the green Trojan/Greek asteroids. The orange regions represent the Hilda asteroids. They form a triangular pattern—why?

The concept of Lagrange points appears multiple times in the novel. This celestial mechanics model explains many behaviors of satellites and asteroids and serves as a mathematical foundation for interstellar travel and space station construction.

Given our understanding of Lagrange points, we know there are Trojan and Greek asteroids corresponding to the Lagrange points L4 and L5 in the Sun-Jupiter orbit. But what about the asteroids positioned directly opposite Jupiter—could they be at L3?





Yes! The equilibrium points of the Hilda asteroids lie at L3, L4, and L5. Unlike the Trojan group, which shares Jupiter’s orbit, Hilda asteroids are located slightly inward. Their triangular distribution is dynamically stable. While each asteroid follows its own orbit, collectively, they maintain a stable triangular formation. Scientists have calculated the ideal orbits of the Hilda asteroids, as depicted below:



(Note: Orange = Sun; Blue = Jupiter; Black and Red = Orbits of two asteroids with eccentricities of 0.310 and 0.211, respectively.)





--- Start of Quote ---

Alcon's Journal # 21
After departing from Galileo#1, we reached the Amalthea supply station—an advanced space platform located on Amalthea itself. This station had a unique feature: a long collection tube that extended into the atmosphere of Jupiter. It was connected to a modified asteroid at Lagrange point L2 of Amalthea, serving as the station's gateway and flight control center. This supply station played a crucial role as the primary hub for humans venturing towards the outer regions of our solar system. In the future, with the establishment of the Uranus supply station, it was expected that humans would embark on exploring and potentially traversing the outer Oort Cloud.

Alcon's Journal # 31
The temperature outside the protective hull of 3137 plunges below minus 200 degrees Celsius. Life here feels delicate and fragile. Due to the abundance of asteroids near Neptune's Lagrange points, most exploration spacecraft steer clear of this region or navigate cautiously at low speeds. I find myself as the sole explorer in this vast expanse.

--- End Quote ---






An interesting real-world example: the recently launched James Webb Space Telescope (JWST) orbits at the Sun-Earth L2 Lagrange point. This location allows JWST to maintain a stable orbit while staying aligned with Earth for data transmission. Additionally, it remains shielded from direct sunlight, enabling its infrared instruments to operate at near-absolute zero temperatures for optimal deep-space observations. L2 was the ideal choice. For NASA’s orbital details, click here: https://webb.nasa.gov/content/about/orbit.html



Orbital Resonance


Orbital resonance is an effect in celestial mechanics where orbiting bodies exert periodic gravitational influences on each other when their orbital periods form a simple integer ratio. The concept is analogous to pushing a child on a swing—both the orbital motion and the swinging have a natural frequency, and when an external force is applied periodically in sync with this frequency, the cumulative effect can either amplify or disrupt the motion. Orbital resonance significantly enhances gravitational interactions between celestial bodies, allowing them to alter or constrain each other’s orbits.

In celestial mechanics, this translates to either a perfectly stable synchronized orbit between two bodies or the destruction of one body's orbit. In most cases involving asteroids, the latter scenario occurs—their orbits are disrupted, causing them to be ejected from their original paths or cleared out, a phenomenon known as “clearing the neighbourhood” or “dynamical dominance”.

Kirkwood Gaps and the Asteroid Belt


In Star Rider, when Alcon first travels to the Kuiper Belt, he must pass through the asteroid belt, where the term Kirkwood Gaps appears:

--- Start of Quote —
Alcon's Journal # 12
Even though we were traveling at a maximum speed of 150,000 kilometers per hour during our last mission, the new engine we installed can now reach speeds of up to 700,000 kilometers per hour. However, maintaining maximum speed through the asteroid belt is not wise, so 3137 will only accelerate in the Kirkwood gap, a relatively sparse region of the asteroid belt that is in resonance with Jupiter's orbit. Whenever we leave the Kirkwood gap and enter an area with a higher concentration of asteroids, we will need to slow down.
--- End Quote ---

A chart of the distribution of asteroid semimajor axes, showing the four most prominent Kirkwood gaps and a possible division into inner, middle and outer main-belt asteroids:



The principle of orbital resonance disrupting asteroid orbits also applies to planetary ring systems, such as the gaps within Saturn’s rings, where resonances have cleared out regions of dust and debris.

Stable Resonances - Laplace Resonance


While resonance can lead to orbital destruction, it can also result in stable orbital configurations. A notable example is the Laplace Resonance among Jupiter’s three moons—Io, Europa, and Ganymede—which have established a stable resonant pattern in their orbits. The following animation illustrates this phenomenon:

Animation of Laplace Resonance:










Gravity Assist - The Slingshot Maneuver


Since gravitational resonance occurs due to a massive planet’s influence on nearby smaller celestial bodies, it also affects passing spacecraft. This principle forms the basis of the gravity assist (or gravitational slingshot) maneuver, which allows spacecraft to gain or lose velocity by utilizing a planet’s gravitational field.

In Star Rider, Alcon explicitly references this maneuver:

In Alcon’s Journal #12, he describes using Saturn for a gravity assist acceleration toward the Kuiper Belt.
In Alcon’s Journal #14, he uses Jupiter for a gravity assist deceleration to reach Galileo I space station, a space station orbiting Jupiter.


The following animation illustrates the concept of gravity assist acceleration which is used by Voyager #1:
 


 

During this process, the most efficient acceleration occurs when propulsion is applied at the velocity peak. This effect is known as the Oberth Effect, which Alcon describes as follows:

--- Start of Quote —
Alcon's Journal # 12
I put my hand with the bracelet on it on the window, and Mars played some ambient music. I lost track of time as we flew by Saturn, and as the ship began to vibrate, Mars increased the engine thrust. We had now departed from the gravity assist trajectory.
Farewell, Saturn, dear father and mother. As we journey onwards, I shall carry you with me as we soar through the stars…
--- End Quote ---


The following animation illustrates gravity assist deceleration (Scenario #d):






Interstellar exploration in the novel frequently employs gravity assist techniques, as they are essential for interplanetary travel. These maneuvers enable spacecraft to conserve vast amounts of fuel, making them a standard practice. Recognizing the cost-saving benefits, the Deep Space Frontier (DSF) command center immediately approved Alcon and Mars’ request for the maneuver:

--- Start of Quote —
Alcon's Journal # 14
With the saved propellant, we can approach Jupiter more closely and save the company money. Moreover, the additional time required occupies my vacation time. The DSF control center almost instantly agrees. Mars shows me the operation permit of the DSF on one screen and makes a face at me on the other screen, saying, "This is the win-win game I have learned."
--- End Quote ---




Tidal Locking


--- Start of Quote —

Alcon's Journal # 18
I looked up at Jupiter hanging in the sky, partly illuminated by the sun like a huge crescent moon that was colorful and constantly changing. Due to gravitational locking, Jupiter appeared fixed in this location from the perspective of the greenhouse's position, but the shadows and bright spots on its surface changed continuously as time passed, depending on the angle at which the sun shone on it. I took off my parents' bracelet from my left hand and put it on my right, then continued to hug Ami tightly from behind.
--- End Quote ---




Tidal locking (also known as synchronous rotation or captured rotation) is a gravitational effect that causes a celestial body to always show the same face to the object it orbits. For example, the Moon is tidally locked to the Earth, meaning we always see the same side of it.

A tidally locked body takes the same amount of time to rotate once on its axis as it does to complete one orbit around its companion. This synchronous rotation causes one hemisphere to remain perpetually facing the partner body. Typically, only the smaller body—such as a moon—becomes tidally locked to a larger planet. However, if two celestial bodies are similar in size and mass, mutual tidal locking can occur, as seen with Pluto and Charon.

The tidal force or tide-generating force is the difference in gravitational attraction between different points in a gravitational field, causing bodies to be pulled unevenly and as a result are being stretched towards the attraction. It results in shape deformations due to mutual gravitational attraction. On Earth, this effect is most visibly seen in ocean tides, though the solid ground also experiences slight bulging. For the Moon, these forces have caused it to become locked with one hemisphere permanently facing Earth. Jupiter’s moon Europa is similarly locked, always showing the same side to Jupiter. Meanwhile, tidal heating occurs through the tidal friction processes: orbital and rotational energy is dissipated as heat in either (or both) the surface ocean or interior of a planet or moon. Due to tidal heating, Europa's interior remains relatively warm, possibly supporting a subsurface ocean. This concept is reflected in Star Rider, where Alcon and Ami dive into Europa's ocean for an adventure.





Warp Drive and Gravitational Wave Detectors


--- Start of Quote —
Alcon's Journal # 8
This famous gravitational wave detection system has been in operation and continuously observing for more than 30 years before being retired. The currently studied curvature propulsion is based on the theory and observation results of this system. According to predictions, it will take more than a decade for the available curvature engines to appear. LISA has been replaced by two sets of equilateral triangle gravitational disturbance detection systems, which are larger and more accurate and use heliocentric orbits. These two sets of equilateral triangles form a huge hexagonal system array named "Beacon I" and "Beacon II". In addition to gravitational disturbance detection, this huge heliocentric system is also used for information relay among various spacecraft, space habitats, and the home planet within and beyond the solar system.
--- End Quote ---

 
Gravitational Wave Detectors - LISA and Beacon I/II


Gravitational waves and warp drive are often related. Let's first explore gravitational wave detection. The principle behind these detectors is similar to the famous Michelson-Morley experiment, where a single beam of light is split into two perpendicular beams, reflected back, and then recombined to create an interference pattern. If the distances in both directions remain unchanged, the interference pattern remains stable. However, if space itself is distorted due to a passing gravitational wave, a phase shift occurs, causing detectable interference.



The first confirmed detection of gravitational waves created a scientific sensation a few years ago. The equipment used was the Laser Interferometer Gravitational-Wave Observatory (LIGO), a large-scale physics experiment and astronomical observatory. LIGO consists of two laser interferometers—one in Hanford, Washington, and the other in Livingston, Louisiana. By comparing data from both sites, researchers significantly reduce the risk of false detections. These interferometers are incredibly sensitive, able to detect minute distortions as small as one-ten-thousandth of a proton’s charge diameter.

The Laser Interferometer Space Antenna (LISA) is another gravitational wave detection project, initially a collaboration between NASA and the European Space Agency (ESA). Due to funding issues, NASA withdrew in 2011, leading ESA to revise the mission and rename it the Evolved Laser Interferometer Space Antenna (eLISA) in 2013. Unlike LIGO, which is Earth-based, LISA consists of a vast equilateral triangle of spacecraft following Earth's orbit, with each side spanning five million kilometers.



LISA is expected to become operational after 2030. In Star Rider, this system has already been retired and replaced by two larger heliocentric equilateral triangles forming a hexagonal detection network. With numerous spacecraft scattered throughout the solar system, some inevitably end up blocked from Earth by the Sun. Thus, this new system serves as both a gravitational wave observatory and a solar system-wide communication relay, akin to ancient China's beacon towers—hence the names Beacon I and Beacon II.





Fusion engine / Propellant-Based Propulsion



--- Start of Quote —
Alcon's Journal # 13
For a vessel like the 3137, which needed to perform exploration missions involving frequent changes in trajectory, acceleration, and deceleration, neither of these futuristic technologies could be used. Instead, we relied on the preliminary practicality of controlled nuclear fusion and the well-established propellant propulsion technology. The gaseous giant planets in the outer solar system, primarily composed of hydrogen and helium, served as excellent materials for fusion engines and a source of propellant. Jupiter and Uranus became our supply stations.
--- End Quote ---


Fusion energy itself isn’t a new concept—the Sun is a massive fusion reactor. Humanity demonstrated nuclear fusion upon detonating the hydrogen bomb, but achieving controlled fusion remains a significant challenge. The most promising approaches involve Inertial confinement fusion (ICF) and magnetic confinement fusion (MCF), though current technology can sustain controlled fusion reactions only for a few seconds or minutes. Recent breakthroughs have extended this duration beyond 1000 seconds, marking a crucial step toward viable fusion power.

For spacecraft propulsion, fusion engines typically use plasma propulsion, where high-temperature plasma is expelled to generate thrust. However, in Star Rider, DSF3137 frequently maneuvers, requiring significant thrust. Plasma-based propulsion, while fast, produces relatively low thrust. Thus, transferring fusion-generated energy into traditional propellant-based thrust would be more effective. Consequently, in the story, the crew often discusses replenishing propellant rather than fuel, as fusion fuel consumption is minimal compared to propellant mass.





Comet Orbits


--- Start of Quote —
Alcon's Journal # 31
During my exploration, I caught sight of another enigmatic comet, yet to be identified. Mars diligently calculated its orbital period to be approximately 12,000 years, given its current trajectory and velocity. Its tail, still indistinct, awaits further clarity. As it ventures beyond the confines of the Kuiper Belt and approaches the inner reaches of the solar system, the comet's material rapidly evaporates, stretching its tail into a resplendent display of luminosity. Perhaps, back on Earth, humans will marvel at its ethereal beauty, unaware that its existence is fleeting. Despite its extended orbital cycle, this celestial wanderer may fade away before it can fulfill its destined lifespan.
--- End Quote ---


As of late 2014, there were 314 officially numbered periodic comets in the solar system. However, unnumbered comets remain poorly documented. Cometary orbits vary widely, ranging from a few years to several million years. Short-period comets originate from the Kuiper Belt, while long-period comets are believed to come from the Oort Cloud. Some comets theoretically have periodic orbits but never complete them due to solar evaporation.

One noteworthy example is Comet 109P/Swift-Tuttle, which has a roughly 133-year orbit. Predictive calculations indicate:

  • In 2126, it will pass 0.153 AU from Earth.
  • In 2261, it will pass 0.147 AU from Earth.
  • In 3044, it may pass as close as 0.011 AU, potentially resulting in an Earth impact.



Cassini-Huygens Saturn Exploration Mission



--- Start of Quote —
Alcon's Journal # 12
After a 20-year exploration mission, Huygens eventually fell silent on Saturn's moon, Titan, while Cassini plunged into Saturn's atmosphere as planned, completing its final observations and self-destruction mission on September 15, 2017, Earth time. As Cassini burned up while passing through Saturn's sky, lined with its massive rings, its story was permanently written into the history of space exploration, even though humans could not witness it with their own eyes.
--- End Quote ---


The Cassini-Huygens mission was a flagship-class space probe sent to explore the Saturnian system, a collaborative project between NASA (National Aeronautics and Space Administration), ESA (European Space Agency), and ASI (Italian Space Agency).

The mission was divided into two main components: Cassini, the orbiter that studied Saturn and its moons, and Huygens, the lander that descended onto Titan, Saturn’s largest moon. The two probes were launched together aboard a Titan IVB rocket on October 15, 1997, and arrived at Saturn in early July 2004. The Huygens probe separated from Cassini on December 25, 2004, successfully landing in the Adiri region of Titan on January 14, 2005. It became the first probe to land on a celestial body in the outer solar system, transmitting data from the surface.

Cassini, meanwhile, continued its mission, orbiting Saturn for over 13 years before finally executing its planned Grand Finale. On September 15, 2017, following mission directives, Cassini plunged into Saturn’s atmosphere, where it burned up, bringing the mission to an end.

Watch a simulation of Cassini's final descent into Saturn's atmosphere (3:55 total length). The final approach begins at 2:45 - https://youtu.be/68vxYRAony8 

 ===============================================

*** Link to "Star Rider": https://www.wattpad.com/story/342470732-star-rider

 



Saturday, September 24, 2022

【星行者】背景知識 - I 太陽系


太陽系,我們的母星系,其大致產生於46億年前的一個星雲的引力坍縮,最終整個星系超過99%的質量都集中在太陽本身,這就是我們的恆星 - 太陽,其剩下的其他物質,則隨著星系的演進陸續形成了各個大小8個行星和行星帶,而這些行星帶,就是【星行者】的主角們進行星際探索的目的地。

對太陽本身來說,由於巨大的質量產生的引力,在太陽的核心,大量的質子(氫原子核)融合成氦原子核,並釋放出高能的x/γ射線,這些高能射線從太陽中心出發,經過上萬年乃至最長達5千萬年之後才能到達太陽表面,並在此過程中被轉換成了可見光和射線的結合體,然後逃逸進入太空,從某種意義上來說,整個太陽系的能量的來源就是來自於太陽的核聚變。

由此不得不說到 “核聚變引擎” 這個詞,在文中反覆出現,這種引擎其實也是採用類似太陽核聚變這樣的技術,而基於這樣的技術水平,整個小說的世界背景便始於此,在那個時代,人類已經開始進行整個太陽系內的探索並由此為能源在多處建造了各種衛星城。

那麼文中提到的各種行星和行星帶,又是什麼樣的呢,木星,土星離我們多遠?小行星帶在哪裡?柯伊柏帶又在哪裡?為什麼Ami和Alcon的任務,動輒就需要幾年?下來就來一一解說。

首先是這張距離比例圖:



看看整個太陽系的大小,這張圖的左邊顯示的是太陽的表面,橫軸表示的是從太陽出發到各個行星的距離的按照比例顯示的位置(可以忽略這個圖中的行星的大小比例,重點關注距離),你可以看到,水星,金星,地球,火星都在最左邊擠成一堆的這幾個紅色豎線的位置,而小行星帶(Asteroid Belt)則在火星和木星之間,劃開了兩個區域,小行星帶左邊的這個區域,成為“太陽系內環 (Inner Solar System)”,這裡面分佈的都是岩石類的行星,地球是第三顆岩質行星,而小行星帶之外,就是木星,土星,天王星,海王星這種氣態巨行星,這個圖的紅色X軸上有2個單位標識,分別是
  • 1.5E8km – 代表 1.5億公里,這是地球到太陽的距離,採用標準計量單位km
  • AU - Astronomical Unit 代表“天文單位”,就是一個地球到太陽的距離,即上述的1.5億公里
有了這個單位的概念之後,你再看上面的圖,就可以看出小行星帶幾乎就是家門口的距離,這也是文中DSF的飛行員們開始進行初階探索的地方,而飛出小行星帶之後,木星大概在5AU的距離,而土星大概在10個AU的距離,到此已經是地球到太陽的10倍距離了,然後到20AU才是天王星,30AU才到海王星,海王星往外再3個AU才開始進入科伊伯帶,文中Alcon的加裝了強大的KU-2級別星際探索引擎的3137,以安全速度飛越每一個AU就需要大約9個地球天,也就是說,即使不做任何躲避直線飛行,飛到海王星甚至還沒摸到柯伊柏帶的邊緣,就已經需要接近300天,所以整個小說的背景中,時間和空間的巨大間隔,構成了故事線中不可或缺的一部分。

上面說明了各個行星和行星帶的距離,下面再說說行星的大小比例,為了展示距離,上述行星的大小並不是按照比例顯示,如果要按照星體的大小比例來顯示,則看起來是這樣的:





從太陽開始,小小的那幾個太陽系內環岩質行星分別是水星(Mercury),金星(Venus),地球(Earth),火星(Mars),看起來,地球真的小的可憐啊,在文中,地球有時候被稱之為 “母星”,這個小小的藍色行星就是我們在宇宙中的家。

文中,在太陽系內環,人類建立了大量的太空城,這樣的太空城基本集中在地-火軌道之間,這個距離到太陽的距離適中,但是可以拿來建造太空城的材料不多,所以家門口的小行星帶就成為了可以提供材料的一個理想場所,這就是整個星際勘探的需求來源。同時,雖然太陽系外環的行星都很巨大,可是他們都是氣態行星,我們人類無法立足,而且太陽系外環的星體遭受小行星和彗星撞擊的可能性都比較大,即便是他們的衛星也不是理想的居住地點。


那麼,衛星城的建立需要的材料可以來自小行星,是否隨便抓到一個都可以用?也不是,按照人類的科技線路,金屬材料憑藉著優異的延展性和可塑性,是最佳的工程材料(或許未來的碳基結構的複合材料也是?可以儘管想像一下)。那麼這種金屬材料可以從小行星帶獲得麼?--- 答案是:可以。


目前太陽系內的小行星按照光譜分析的結果大致有幾種(數量少的就不說了,主要是這3類)

  • C-型小行星:占所有小行星的75%,數量最多,基本是碳元素。
  • S-型小行星:占所有小行星的17%,主要成分包括鐵、鎂和矽。
  • M-型小行星:剩下的小行星中大多數屬於這一類,鎳,鐵成分居多,一般說法是以前行星的金屬核的殘片或者殘留。

文中也提出,C/S類別的小行星的改造技術還在研究中,而最常用的就是M型小行星,這也是Ami和Alcon等飛行員勘探尋找的目標,而在他們識別安裝了追蹤裝置之後,這種小行星就成為他們所在公司的資產,勘探飛船負責勘探和標識,然後會有牽引飛船(類似我們的拖船)來把行星拖到目的地進行開採和改造。

相對於“家門口”的小行星帶,柯伊柏帶(Kuiper Belt)就是一個位於海王星軌道之外遙遠的小行星帶,而且有些行星的塊頭還不小,比如被降級的冥王星,它就是柯伊柏帶的一個矮行星,文中也提及,因為距離非常遙遠並且範圍巨大,勘探成本也高很多,危險也無處不在,如果從經濟利益上來說,回報率並不高,所以在這個區域進行的勘探的性質其實更像圈地運動。而Alcon,應該就是第一批進入柯伊柏帶勘探的飛行員,在文中,他們被稱之為 “ 拿到KU-2認證 ” 或者 “KU-2級別” 的飛行員。

在這裡,先放一個位於火星和木星之間的小行星帶的黃道面俯視圖,你會發現,這些小行星的佈局好像有些規律?是的,整個太陽系的行星之間的引力相互作用會產生很多有趣的效應,在下一篇文章中,我會來說說太陽系中的各個行星和行星間的行星力學導致的一些有趣現象:




Friday, September 23, 2022

【星行者】 背景知識 - II 拉格朗日點

天體力學中有一個很重要的力學解,就是 “拉格朗日點”, 維基百科的解釋是:拉格朗日點(Lagrangian point)又稱平動點(libration points)在天體力學中是限制性三體問題的五個特殊解(particular solution)。

簡單點說,就是當2個巨大的天體進行軌道運動的時候,會產生另外5個平衡點,實現其他小天體在這個平衡點或者基於這個平衡點實現動力學上的平衡,很多回答說這個是“三體” 的解,但是其實不算,三體中3個星球的質量類似,而在拉格朗日點的概念中,重點是“2個巨大的天體,和一個/一堆可以認為不影響引力環境的小天體” 形成的平衡,這裡特別說明第三個必須是 “足夠小” 。

拉格朗日點的簡化圖示就是如下的樣子,兩個巨大的天體形成的引力和動力環境中,有數字標識的1-5總共5個平動點,我們一般稱之為L1,L2,L3,L4,L5,對應下圖的1~5,在這5個點上的小星體可以比較“舒服”的呆著或者圍繞著對應的點運動。



回頭看下我們的太陽系,太陽佔掉了99.86%的比重,木星比其他所有行星加一起的質量還要大2.5倍(參照以下的行星質量表,來源:NASA),那麼,我們就可以用拉格朗日點的概念來套用解釋小行星帶(Asteroid Belt)的小行星們的運動。

行星
水星
金星
地球
火星
木星
土星
天王星
海王星
冥王星
質量(1024kg)
0.330
4.87
5.97
0.642
1898
568
86.8
102
0.0130


上一章的結尾我們用了一張小行星帶的黃道面的俯視圖,先把這張圖簡化一下,就是這個樣子:



首先位於火星(Mars)和木星(Jupiter)之間的白色環狀帶是小行星主帶(Main Asteroid Belt),這個小行星帶因為離家近,剛過火星軌道不遠就到了(其實說近...還是在2AU之外),這就是DSF的飛行員門的初階練習場,但是你再往外一點,在外面一圈的木星軌道上(木星在右下角,標識 Jupiter),還有2群小天體,上圖標識為 “Trojan Asteroids” (特洛伊群),等等!他們...為什麼是用的木星軌道!?

是的,他們就是和木星共用軌道,分別座落於L4,L5的特洛伊群小行星,其實L4的還有一個名字叫“希臘族”小行星(Greeks),只是早期大家還沒把特洛伊群分的那麼清楚,後來發現多了成堆了,才開始用 “希臘族/希臘營” 命名,但是因為早期命名已經亂了,所以常常出現希臘族裡面出現特洛伊英雄的名字命名的小行星,或者特洛伊群裡面出現希臘英雄的名字命名的小行星,反正你記住他們就是位於太陽-木星的L4/5 拉格朗日點上,和木星共用軌道的小行星群就對了。

== #章節引用 “#Alcon自述12”# =====
最終脫離小行星主帶之後,還會需要進行最後一次大推力機動調整到相對稀疏的安全脫離區域, 這個安全脫離的區域除了要求能盡量利用未來航線上別的行星的引力加速,還需要並避開 位於太陽-木星 拉格朗日點上聚集的 希爾達族小行星群(Hilda asteriods )和特洛伊小行星群( Trojan asteroids)。 

Mars評估了下,這次補充的工質足夠,即使需要這麼多的機動動作也有足夠餘量,但是這次木星也不在我們的航線相遇的位置,所以我們會直接飛越木星軌道,由於我們需要機動避開和木星共軌的特洛伊群小行星,屆時木星,利略衛星城和木衛五改造的補給站都在蠻遠的距離,而且有一堆小天體群擋著或者直接就在木星身後無法被我觀測到
==  # 章節引用結束# =====

所以在Alcon的第一次前往柯伊柏帶的勘探途中,要安全穿越小行星帶,Mars計算了一條線路來避開聚集的小行星們,那麼,這裡又提及了一個小行星群 - 希爾達族小行星群(Hilda asteriods ),這些又是什麼小行星群?


現在讓我們回來看一下上一章節的比較複雜的小行星帶的黃道面俯視圖,白色的小行星主帶,綠色的特洛伊/希臘群你應該都已經熟悉了,那麼這些橙色的就是希爾達小行星群,看起來是一個三角形的分佈,看過了拉格朗日點的概念,你應該可以猜得出靠近特洛伊和希臘群的就是位於L4,L5的,但是和木星(Jupiter)隔日相望的....難道是拉格朗日點 L3?




是的,希爾達群的平衡點就是分別位於L3/4/5 三個拉格朗日點,他們的位置比特洛伊群更靠裡面。而且,這個三角形是一個動態穩定的三角形,也就是每個小行星都有自己的軌道但是動態形成了一個比較穩定的三角形,科學家門計算的理想的希爾達族小行星的軌道是這樣的:

注:橙點:太陽;藍點:木星,黑色和紅色分別為偏心率(eccentricity) 取值為 0.310 和0.211的兩個小行星的軌道。





拉格朗日點的概念在整個文章中出現過多次,這種行星動力學模型解釋了很多衛星和小行星的行為,也成為星際航行和空間站建造的一個數學理論基礎:

== #章節引用 “#Alcon自述21”# =====

離開伽利略1號不久,我們就抵達了木衛5補給站,這是一個基於木衛5建立的多功能補給中心,一根長長的採集管從木衛5伸入木星大氣,然後在木衛5 遠離木星方向的拉格朗日點連結了一個改造的小行星作為補給站的渡口和補給站飛行控制基地,這裡是人類飛往太陽系外環的最重要的補給站,幾年之後,當天王星補給站建立,那時候的人類應該已經開始探索甚至嘗試穿越更外層的奧爾特星雲(Oort cloud)了吧。

== #章節引用 “#Alcon自述31”# =====

而此時3137的艙體外層,溫度是零下200 多度,在這裡,生命是如此脆弱,由於海王星的拉格朗日點附近聚集了比較多的行星,勘探飛船會盡量避開這一帶或者只能以低速運行,我是這附近唯一的一艘勘探飛船

==  # 章節引用結束# =====

另一個有趣的故事:前段時間發射的詹姆斯.韋伯望遠鏡(James Webb Telescope)就是基於太陽/地球的L2 拉格朗日點運動,除了要跟隨地球好進行數據通訊,以及需要盡量遠離太陽的直射以便它的各種紅外探測儀器能在接近絕對零度的環境觀察整個宇宙,還能實現用最小的能源動力就能跟隨地球進行運動,L2點成為最佳的選擇。NASA的軌道說明請點擊此連結:
https://webb.nasa.gov/content/about/orbit.html 



一個問題: 在日-地系統中,地球有沒有對應L4/5的特洛伊小行星?(Google一下你會發現有趣的答案)




 

Thursday, September 22, 2022

【星行者】背景知識 - III 軌道共振&引力彈弓

 軌道共振在維基百科上的定義:

轨道共振是天体力学中的一种效应与现象,指当轨道上的天体于周期上有简单(小数值)的整数比时,定期施加的引力影响到对方所产生的。其物理原理在概念上类似于推动儿童荡的秋千,轨道和摆动的秋千之间有着一个自然频率,其它机制和“推”所做的动作周期性地重复施加,产生累积性的影响。轨道共振大大增加了相互之间引力影响的机构,即它们能够改变或限制对方的轨道。


再類比回秋千的例子,最後的結果要麼是秋千的節奏被打破,共振消失,要麼就是進入一種穩定的共振狀態,換到天體力學上來說,就變成相互的軌道之間,要麼完美的進入一種協振穩定的狀態,或者其中一方的軌道被摧毀,而發生在小行星 身上的更多是第二種情況,即軌道被摧毀,被大的星體彈出去了,或者被稱為“清空”。


在小說中,Alcon在第一次前往柯伊柏帶的旅程中,需要穿越小行星帶,這裡面出現了一個詞 “柯克伍德空隙( Kirkwood gap)”:


== #章節引用 “#Alcon自述12”# =====


對於上次最高速度15 萬公里每小時的我們,進入小行星帶依然覺得無比空曠,但是這次我們更換了引擎之後時速最高可達70萬公里,在這樣的動力條件下繼續保持最高速度穿越就不是明智的選擇,因此Mars只有在小行星主帶和木星軌道共振形成的 柯克伍德空隙內( Kirkwood gap)會盡量加速,但是離開柯克伍德空隙進入充滿密集星體的軌道的時候就必須減速


==  # 章節引用結束# =====


看一下下面的小行星主帶的行星軌道分佈圖,橫坐標為共振係數,縱座標為小行星數量,就可以發現,這些位於虛線標識的整數比例的共振帶上的小行星的軌道基本上都被摧毀了,導致形成了這些位置都是空白,這就是柯克伍德空隙的由來:




上面說的是小行星的軌道被共振摧毀,包括一些星環塵埃也適用這樣的規則,比如土星環間形成的間隙,這些都是軌道被清空的例子。


而對於一些不小的天體,形成穩定的共振也是一種情況,比如木星的3個衛星(艾奥-欧罗巴-佳利美德)完美的形成各自穩定的軌道,如下面的動圖所示,這種共振又被稱之為 “拉普拉斯共振”:




引力共振既然是大的行星的引力對鄰近軌道上的其他小天體產生了牽拉,那麼這種引力也會對飛越附近的探測器和飛船產生影響吧?那麼我們是否可以加以利用呢?答案是肯定的,這就是“引力彈弓(重力助推)”的由來。


小說的 “ Alcon自述#12 ” 專門說到了用土星進行引力彈弓加速前往柯伊柏帶,以及在回程的時候(Alcon自述#14),利用木星進行引力彈弓減速前往伽利略一號衛星城,這裡面分別描述到了加速和減速兩個場景,文字的描述可能不如動圖來的清楚,可以看這兩個動畫:


這個動圖是利用引力彈弓加速的示意,灰色球體為用來產生彈弓效應的天體,小藍點為人類飛行器,座標軸為時間和速度的關係:



在加速過程中,加速最大效率是在速度拱點的時候進行動力加速脫離,這種效應又被稱為“奥伯特效应” ,Alcon的描述是這樣的:


== #章節引用 “#Alcon自述12”# =====

我把戴著手環的手放在窗前,Mars放起了一段應景的環境音樂,不知過了多久,隨著船體的顫動,Mars加大了引擎推力,我們已經進入引力彈弓的脫離航線了,再見,土星,父親母親,我們繼續前行,我帶你們去飛越星辰...

==  # 章節引用結束# =====



這個動圖則是利用引力彈弓減速的示意:





小說中的星際勘探,用到彈弓效應(重力助推)的場景比較多,這也是星際航行中常見的加減速手段之一,也可以減少大量的燃料使用,所以DSF幾乎是立刻同意了Alcon和Mars的請求:


== #章節引用 “#Alcon自述14”# =====


因為引力彈弓減速節省的推進工質可以為公司省錢,而且所需要的額外時間佔用的是我的休假時間, DSF控制中心幾乎是秒回同意了,Mars一邊給我顯示著DSF的操作許可,一邊在顯示終端上給我打了一個鬼臉並補充:“這是我學會的雙贏博弈。 ”


==  # 章節引用結束# =====


Wednesday, September 21, 2022

【星行者】背景知識 - IV 其他名詞解釋

 潮汐锁定

==# Alcon自述 -18 #==

我望著木星懸掛在天空,一部分被太陽照亮著像一輪巨大的彎月,而且是色彩豐富變幻的彎月,由於潮汐鎖定,這個溫室所在的位置看到的木星始終是固定在這個位置,只是太陽照著木星的角度形成的木星表面的陰影和亮面隨著時間持續變幻著,我把父母親的手環摘下來換到右手,然後繼續把右手放在Ami 背後摟緊她。 

==  # 章節引用結束# ==

維基百科上的定義是:潮汐鎖定(或同步自轉、受俘自轉)發生在重力梯度使天體永遠以同一面對著另一個天體;例如,月球永遠以同一面朝向著地球。

潮汐鎖定的天體繞自身的軸旋轉一圈要花上繞著同伴公轉一圈相同的時間。這種同步自轉導致一個半球固定不變的朝向夥伴。通常,在給定的任何時間裡,只有衛星會被所環繞的更大天體潮汐鎖定,但是如果兩個天體的物理性質和質量的差異都不大時,各自都會被對方潮汐鎖定,這種情況就像冥王星與凱倫。

這裡面的“重力梯度”又稱為潮汐力,也就是引力相互引起的一些形變,對地球來說比較明顯的就是海水被拉高了形成潮汐,其實地球的地面也被拉起來了只是感覺不明顯,而對於月球來說就會比較明顯導致月球被鎖定一面始終朝著地球,木星的歐羅巴也是處於這種情況,永遠以同一面面對著木星,而且因為歐羅巴內部受潮汐加熱效應,可能會表現為相對溫暖的地表下的海洋,所以故事中也有Alcon和Ami潛入歐羅巴的海洋去遊玩的描述。



曲率引擎

 ==# Alcon自述 -8 #==

這套著名的引力波探測系統 (LISA) 已經運行並持續觀測了30多年後退役了,目前正在研究的曲率推動就是基於理論和這套系統的觀測結果,而可用的曲率引擎根據預測還需要十幾年才會出現。

==  # 章節引用結束# ==

引力/重力波探測器 - LISA 和 烽火 I / II 

 ==# Alcon自述 -8 #==

取代LISA的是更龐大更精確的的採用的日心軌道的2套等邊三角形引力擾動探測系統,而這兩套等邊三角形的系統也組成一個巨大的六邊形系統陣列,這套巨大的日心系統被命名為“ 烽火I“ 和 “烽火II" ,除了引力擾動探測,也用於目前的太陽系內外各個飛船,衛星城和母星之間的資訊中繼。 

==  # 章節引用結束# ==


重力波/引力波和曲率引擎始終是在一起的話題,先說引力波的探測,這個探測器的原理類似於最早的邁克爾遜.莫雷 實驗,就是讓一束光經過分光器之後分別往兩個方向前進,然後被反射回來進行干涉,如果這兩個方向的距離沒有形變,那麼干涉結果就是相互抵銷,而一旦一個方向上的長度發生了變化(也就是空間被扭曲了),就會形成相位差,在偵測器上產生干涉,因此感應到重力波。

邁克爾遜.莫雷實驗圖示:



前幾年人類探測到引力波曾經引發了一大波熱潮,這背後所用的設備就是 雷射干涉引力波天文台(英語:Laser Interferometer Gravitational-Wave Observatory,縮寫:LIGO)是探測引力波的一個大規模物理實驗和天文觀測台,其在美國華盛頓州的漢福德與路易斯安那州的利文斯頓,分別建有雷射干涉儀。利用兩個幾乎完全相同的干涉儀共同進行篩檢,可以大幅度減少誤判假引力波的可能性。[1]干涉儀的靈敏度極高,即使臂長為4千米的干涉臂的長度發生任何變化小至質子的電荷直徑的萬分之一,都能夠被精確地察覺。


而激光干涉太空天線(Laser Interferometer Space Antenna,LISA)是一個由美國太空總署(NASA)和歐洲太空總署(ESA)合作的重力波探測計劃,由於募款問題,美國太空總署於2011年宣佈終止合作關係。歐洲太空總署因此修改任務概念,於2013年宣佈改名為演化激光干涉太空天線(Evolved Laser Interferometer Space Antenna,eLISA),其實原理和LIGO差不多,就是變成一個跟著地球走的超大等邊三角形空間探測器,每個三角形的邊長是 5百萬公里:

LISA系統圖示:



LISA這套系統預計是在2030年之後才會投入使用,小說中說這套系統已經退役了,取而代之的是另外2套更巨大的環繞太陽的系統,其實就是2個等邊三角形的系統,形成一個六邊形的系統,而那時候的星際勘探很多飛行器會廣泛分佈在整個太陽系內,必然會有一部分和地球之間會被太陽隔開,那麼這個系統既是引力波探測器又用於太陽系內通訊中繼,類似中國長城上的烽火傳訊,因此被命名為 烽火 I / II 兩套系統。

而由引力波衍生出來的曲率推進技術,類似於人工在空間中建立彎曲或者落差,進而推動物體前進,但是本身這個技術在目前還是處於理論階段,在小說中也說明了即使在核聚變已經成熟的時代,也只是抵達了能夠造成空間微小形變的能力,更多像是一種實驗性質的成果,在那時候還需要幾十年後才會出現成熟的曲率推進技術。


核聚變約束/工質推進

==# Alcon自述 -13 #==

對於3137這種需要執行勘探任務的飛船,需要頻繁改變航線和加減速甚至啟停,無法採用這兩種代表未來的技術,只能使用初步實用化的可控核聚變和已經非常成熟的工質推進技術,而外太陽系的氣態巨行星基本上是氫氣和氦氣為主構成,則成為絕佳的聚變引擎的材料和推進工質來源,木星和天王星的補給站便應運而生。

==  # 章節引用結束# ==


核聚變其實不是什麼新概念,太陽本身就是一個巨大的核聚變工廠,而人類在引爆氫彈的那一刻已經宣告可以“造成核聚變”,但是,這個和“可控核聚變” 還離的很遠,要拿來做核聚變引擎,“可控”是關鍵,目前比較可實現的技術是慣性約束和磁性約束,但是也只是能實現幾秒或者幾十秒的可控時間,最近的新聞是可以維持超過1000秒了,這也是未來的能源發展方向。

那麼對於核聚變引擎,在太空中作為飛行器的動力,一般比較常見的思路是採用核聚變產生的等離子體進行推進,但是小說中提及,勘探飛船需要大量的機動飛行動作,所以,等離子體雖然溫度高速度快但是相對推力還是小了點,對於需要大量機動的飛行器,採用核聚變來把能量轉移到傳統推進工質並噴出的效果可能會遠超等離子體,所以文中大部分的描述都是說在 “補充工質” 而不是“補充燃料”,雖然核聚變也需要原料,但是比起推進工質的量還是少的多得多。


彗星週期

==# Alcon自述 -31 #==

在這裡,我又見到了另一顆不知名的彗星,Mars計算出它的公轉週期如果按照這個角度和速度,大概是1萬2千年,它的彗尾還沒那麼明顯,隨著它離開柯伊伯帶深入太陽系核心,物質迅速揮發拉長彗尾,會在沿途拉出一道長長的光芒, 在母星上的人類或許會讚美它的美麗,而它的生命也會迅速消退,對它來說,縱然有著1萬2千年的週期,可是它可能連一次完整的生命都沒有走完就已經消失殆盡...

==# Alcon自述-13- #==

Mars提醒我不久以後可以看到 斯威夫特-塔特爾彗星(109P/Swift-Tuttle),這是一顆周期大約133年的彗星,而且幾千年後可能會非常接近甚至撞擊地球或者月球,因為距離比較遠而且可以位於在 3137前方,Mars建議不停止離心力以節省工質,直接觀測即可

==  # 章節引用結束# ==


截至2014年末,太陽系內擁有永久編號的週期彗星共有314顆。但是對於未編號的彗星,其實我們的紀錄比較零散,彗星的軌道週期範圍也很大,可以從幾年到幾百萬年。短週期彗星來自超越至海王星軌道之外的柯伊柏帶。長週期彗星被認為起源於奧爾特雲,主要由冰凍天體構成的球殼。長週期彗星受到路過恆星和銀河潮汐的重力攝動而直接朝向太陽前進。雙曲線軌道的彗星可能在進入內太陽系之前曾經被沿着雙曲線軌跡被拋射至星際空間,則只會穿越太陽系一次。所以,有些彗星,即使有這所謂的理論週期,但是在路上就被太陽蒸發殆盡是常有的事情。

109P/Swift-Tuttle 這個彗星有興趣的讀者可以查詢一下,幾個測算顯示:

2126年會在離地球大概0.153AU的地方掠過

2261年會在離地球大概0.147AU的地方掠過

3044年會在離地球大概0.011AU的地方“掠過”(或許這時候就會撞上了)



卡西尼-惠更斯號(Cassini–Huygens)土星探測計劃

==# Alcon自述 - 12 #==

“經過20年的探測任務,惠更斯號最終長眠於土衛六,而卡西尼號則按計劃沖入土星大氣完成最後的觀測和自我銷毀任務, 地球時間2017年9月15日,卡西尼劃過映襯著巨大的土星環的土星天空,一路燃燒殆盡”

==  # 章節引用結束# ==

卡西尼-惠更斯號(英語:Cassini–Huygens)是前往土星系統的一架旗艦級太空探測器,也是由美國國家航空暨太空總署(NASA)、歐洲太空總署(ESA)和義大利太空總署(ASI)合作進行的任務。

整個任務分為兩部分:環繞土星的卡西尼號(Cassini)與在土星最大衛星土衛六登陸的惠更斯號(Huygens)。兩具探測器由泰坦四號B型運載火箭搭載,於1997年10月15日一同發射升空,並於2004年7月初抵達土星軌道,隨後在同年12月25日分離。惠更斯號於2005年1月14日成功於土衛六的阿迪立地區著陸並傳回數據,是首具在外太陽系天體完成登陸的探測器。

而卡西尼號自入軌後持續運作超過13年,直到2017年9月15日按照指令操作進入土星大氣層焚毀。

卡西尼號墜入土星大氣層的模擬視頻,總長3:55,從2:45開始講述最後的進入,任務至此終結: