SpaceX Falcon9

-

SpaceX Falcon 9

Falcon 9 is a partially reusable, human-rated, two-stage-to-orbit, medium-lift launch vehicle designed and manufactured in the United States by SpaceX. That says wikipedia. Let's go deeper into it. 

Falcon 9 is a reusable, two-stage rocket designed and manufactured by SpaceX to transport of people and payloads into Earth orbit and hopefully beyond. Falcon 9 rocket is the first orbital class of reusable rocket that flies to ISS and other private programs. It helps to reduce to price and cost of the flight of the rocket, as it is used again for the next plan helping the space game open to broader context.

The first Falcon 9 launch was on 4 June 2010, and the first commercial resupply mission to the International Space Station (ISS) was launched on 8 October 2012. In 2020, it became the first commercial rocket to launch humans to orbit to ISS. 



The height of the Falcon 9 is 70 m and diameter is 3.7 m. Mass is 549,054 kg. 

The rocket has two stages. The first (booster) stage carries the second stage and payload to a pre-determined speed and altitude, after which the second stage accelerates the payload to its goal orbit. The booster is capable of landing vertically to facilitate reuse. This feat was first achieved on flight 20 in December 2015. As of 28 September 2024, SpaceX has successfully landed Falcon 9 boosters 338 times. Individual boosters have flown as many as 23 flights. Both stages are powered by SpaceX Merlin engines, using cryogenic liquid oxygen and rocket-grade kerosene (RP-1) as propellants.

Falcon 9 is a two-stage rocket designed and manufactured by SpaceX. It transports satellites and Dragon to the Earth's orbit. In order to protect the satellites on the way to the orbit they are covered by the carbon composite material fairing. The fairing is jettisoned about 3 minutes into the flight. Those fairings are usually recovered to be used again in the next mission.  

SpaceX Merlin 1A, Source: Wiki

Falcon 9’s first stage incorporates nine Merlin engines and aluminum-lithium alloy tanks containing liquid oxygen and rocket-grade kerosene (RP-1) propellant  in a gas-generator power cycle. Merlin is a family of rocket engines developed by SpaceX. They are currently a part of the Falcon 9 and Falcon Heavy launch vehicles, and were formerly used on the Falcon 1.
These engines are gimbaled and have throttle and restart capability for high degrees of control. They are build that way that even two of the nine Merlin engines in the first stage can malfunction without affecting the launch. 
The LOX/RP-1 turbopump on each Merlin engine is powered by a fuel-rich open-cycle gas generator similar to that used in the Apollo-era Rocketdyne F-1 engine.
The current models are Merlin 1D (M1D) for sea-level and Merlin 1D Vac (MVac) for vacuum. 

Gas-generator rocket cycle. Source: Wiki

Falcon 9 generates more than 7,607kN of thrust at sea level and 8,227kN of thrust in vacuum. 

The first (booster) stage carries the second stage and payload to a predetermined speed and altitude, after which the second stage accelerates the payload to its target orbit. The booster is capable of landing vertically to facilitate reuse. Falcon 9's Interstage is a composite structure that connects the first and second stages, and houses the pneumatic pushers that allow the first and second stage to separate during flight. Falcon 9 is equipped with four hypersonic grid fins positioned at the base of the interstage. They orient the rocket during reentry by moving the center of pressure.

Here are the Falcon9 grid fins. source: Grid Fins & Rocket guidance (spaceandscience.fr)

Grid fins (or lattice fins) are a type of flight control surface used on rockets and bombs, sometimes in place of more conventional control surfaces, such as planar fins. They were developed in the 1950s by a team led by Sergey Belotserkovskiy. Grid fins have also been used on specialized devices such as part of the launch escape system for the Soyuz spacecraft.

In 2014, SpaceX tested grid fins on a first-stage demonstration test vehicle of its reusable Falcon 9 rocket, and on December 21, 2015 they were used during the high-velocity atmospheric portion of the reentry to help guide a commercial Falcon 9 first stage back to land for the first successful orbital booster landing in spaceflight history.

The second stage of Falcon 9 is powered by a single Merlin Vacuum Engine, delivers the payload to the  Earth's orbit. The second stage engine ignites a few seconds after stage separation. They can deliver multiple payload to different orbits on the same flight. The second stage Merlin engine generates 981kN of thrust in vacuum. 

Payload is either satellites covered by the fairing or Dragon, which is capable of delivering up to 7 astronauts to the space. 

I guess that the most notable mission was the Crew Dragon Demo-2 test flight. The spacecraft got the name Endeavour, and it was launched on 30 May 2020. Falcon 9 carried NASA astronauts Doug Hurley and Bob Behnken to the International Space Station. It was the first crewed mission from US since the last Space Shuttle mission in 2011. Also it was the first private operated mission by SpaceX. 

Patch of the Crew Dragon Demo-2, source: Wiki



Comments

Post a Comment

Popular posts from this blog

Apollo 8 delta-v calculation

-
Image
The Apollo 8 Apollo 8 mission launched on December 21, 1968, and it was the second crewed spaceflight mission flown in the Apollo space program. The first mission, Apollo 7, stayed in Earth orbit. Apollo 8 mission was the first ever mission to leave the Earth's gravitational sphere, and to reach the Moon. The crew orbited the Moon ten times and returned home. It went without the landing. However, the mission was the first mission to see and take a photo of the far side of the Moon.  The mission consisted of three astronauts: Frank Borman, James Lovell, and William Anders.  Apollo 8 was the third flight and the first crewed launch of the Saturn V rocket.  Earthrise: Taken from Apollo 8; source: Wiki When building a rocket, it is a good thing to do staging. Staging basically means throwing away big, expensive parts of your rocket while the rest continues on the way up. The main advantage is not to carry dead weight.  When one has multiple powered stages, the question a...
Read more

Exercise on single stage vs. two-stage rocket

-
Image
Exercise: 1. Single stage rocket:  Before a rocket begins to burn fuel, the rocket has a mass of  m r,i =2.81×10 7 kg, of which the mass of the fuel is  m f,i =2.46×10 7 kg. The fuel is burned at a constant rate with total burn time is 510 s and ejected at a speed v e = 3000 m/s relative to the rocket. If the rocket starts from rest in empty space, what is the final speed of the rocket after all the fuel has been burned? What we know: initial rocket mass m r,i =2.81×10 7 kg initial mass of the fuel m f,i =2.46×10 7 kg t = 510 s v e  = 3000 m/s So, we can calculate the dry mass of the rocket m r,d =m r,i -m f,i =0.35×10 7 kg. The mass ratio is then R = m r,i  /m r,d =8.03. So, the final speed of the rocket is then: V r,f =Δv r =v e lnR=6250m/s. 2. Two-stage rocket:  Now, we have similar example, the same rocket as in the previous example, but the fuel will be burnt in two stages ejecting the fuel in each of the stages at the same relative speed (v e  =...
Read more

Specific impulse

-
Image
Specific impulse  I was many times using the term specific impulse. So, let's speak about it in more detail.    Specific impulse (usually abbreviated I sp ) is a measure of how efficiently a reaction mass engine, such as a rocket using propellant or a jet engine using fuel, generates thrust. A propulsion system which has a higher specific impulse uses the mass of the propellant more efficiently than a propulsion system with lower specific impulse. Now, in the case of a rocket, this means less propellant is needed for a given delta-v, so that the vehicle attached to the engine can more efficiently gain altitude and velocity. For all vehicles specific impulse (impulse per unit weight-on-Earth of propellant) in seconds can be defined by the following equation: Thrust is force, the thrust obtained from the engine (newtons or pounds force), g 0 is the standard gravity, which is nominally the gravity at Earth's surface (m/s2), I sp is the specific impulse measured (secon...
Read more