The hurdles that face a spacecraft during its launching

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Discussion Overview

The discussion centers around the various stresses and challenges that a spacecraft encounters from the moment of launch until it reaches orbit. Participants explore the physical forces, vibrations, and acoustic environments that affect spacecraft during this critical phase, as well as historical examples of specific incidents related to these challenges.

Discussion Character

  • Exploratory
  • Technical explanation
  • Historical

Main Points Raised

  • Some participants note that huge inertial forces during launch can cause significant shaking of the spacecraft, with differential forces affecting different parts of the vehicle.
  • One participant mentions that astronauts have described the experience of launch as akin to being on the end of a whip antenna, highlighting the flexibility and lightweight construction of the craft.
  • Another point raised is the impact of acoustic noise and vibration profiles that payloads must endure during launch, with references to specific user guides for launch vehicles like Falcon 9 and Atlas V for further details.
  • A historical example is provided regarding the Saturn V rocket, where the center engine experienced violent oscillations that led to an early shutdown during the Apollo 13 launch to prevent damage to the vehicle.

Areas of Agreement / Disagreement

Participants generally agree on the types of stresses faced by spacecraft during launch, but there are multiple perspectives on the specific effects and historical incidents, indicating that the discussion remains open and exploratory.

Contextual Notes

Some limitations include the dependence on specific launch vehicle designs and the varying conditions of different missions. The discussion does not resolve the complexities of the interactions between various forces and the structural responses of spacecraft.

Cerdocyon
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Hello,
My question is quite simple.
What kind of abuses does a spacecraft sustain from the moment it's launched until it's placed on orbit?I've always heard of what a spacecraft must face in the spatial environment but I've never heard of what it must face before it gets to it.
Thank you.
 
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There are huge inertial forces affecting a craft during launch - which shakes the crap out of it. A large craft is affected by differential forces across the length of the vehicle. The 'passenger' capsule is usually mechanically isolated from the launch vehicle for this reason.
 
Cerdocyon said:
Hello,
My question is quite simple.
What kind of abuses does a spacecraft sustain from the moment it's launched until it's placed on orbit?I've always heard of what a spacecraft must face in the spatial environment but I've never heard of what it must face before it gets to it.
Thank you.

One of the astronauts said it was like being on the end of a whip antenna. The craft is built lightly and is flexible.
 
Different launch vehicles have acoustic noise and vibration profiles that the payload (say, a satellite or crew capsule) has to endure during launch. As an example, you can look at the Falcon 9 Payload User's Guide [1] or the Atlas V User's Guide [2]. If you want to dig up some more profiles yourself, a search for "acoustic noise and vibration of launch vehicles" [3] may give you some ideas of what is involved.

[1] http://www.spacex.com/Falcon9UsersGuide_2009.pdf
[2] http://www.ulalaunch.com/site/docs/product_cards/guides/AtlasVUsersGuide2010.pdf
[3] http://www.google.dk/search?q=acoustic+noise+vibration+launch+vehicle
 
Last edited by a moderator:
Ok thank you for your answers, it helped me a lot.
 
Something interesting to note is that the center engine on the Saturn V rocket was subject to such violent oscillations that it actually had to turn itself off on the Apollo 13 launch to avoid tearing apart the launch vehicle.

The mission was launched at the planned time, 02:13:00 PM EST (19:13:00 UTC) on April 11. An anomaly occurred when the second-stage, center (inboard) engine shut down about two minutes early. The four outboard engines and the third-stage engine burned longer to compensate, and the vehicle achieved very close to the planned circular 100 nautical miles (190 km) parking orbit, followed by a normal translunar injection about two hours later.[8][5] The engine shutdown was determined to be caused by severe pogo oscillations measured at a strength of 68 g and a frequency of 16 hertz, flexing the thrust frame by 3 inches (76 mm). The vehicle's guidance system shut the engine down in response to sensed thrust chamber pressure fluctuations. Pogo oscillations had been seen on previous Titan rockets, and also on the Saturn V during Apollo 6,[9] but on Apollo 13 they were amplified by an unexpected interaction with turbopump cavitation.[10] Later missions implemented anti-pogo modifications that had been under development. These included addition of a helium gas reservoir to the center engine liquid oxygen line to dampen pressure oscillations, an automatic cutoff as a backup, and simplification of the propellant valves of all five second-stage engines.
http://en.wikipedia.org/wiki/Apollo_13#Launch_and_translunar_injection
 
Huh, knew it had lost an engine, never heard why before, thanks.
 

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