Breaking Bonds in Space: Understanding UV Radiation's Effects on Covalent Bonds

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Discussion Overview

The discussion revolves around the effects of UV radiation on covalent bonds in space, specifically focusing on which bonds can be broken, the rate of loss of Kapton film due to atomic oxygen, and the time required for a window to be covered by oxygen at high altitudes. The scope includes theoretical and homework-related aspects.

Discussion Character

  • Homework-related
  • Technical explanation

Main Points Raised

  • One participant suggests that covalent bonds such as O-O, N-N, C-N, C-C, C-O, and double pi bond C=C can be broken by UV radiation in space.
  • Another participant poses a question regarding the rate of loss of Kapton film thickness due to atomic oxygen, providing specific values for flux and reaction efficiency.
  • A third participant inquires about the time required for a 1m2 window to be covered by O2 at an altitude of 300km, referencing a specific adsorption rate equation.
  • There is a suggestion to produce certain objects in space rather than on Earth, although no specific examples are provided.

Areas of Agreement / Disagreement

Participants have not reached a consensus on the specific bonds affected by UV radiation or the calculations related to the rate of Kapton film loss and oxygen adsorption. Multiple competing views and questions remain unresolved.

Contextual Notes

Participants are required to show attempts at solving homework problems before receiving assistance, indicating a focus on individual problem-solving rather than collective resolution.

ania 5555
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Please can you help me with these question;

1)Which bonds can be broken by UV radiation in space?

I've done it but I'm not sure if this is correct.
Covalent bond can be broken by UV radiation in space such as; O-O, N-N, C-N, C-C,
C-O, and double pi bond C=C

2)Consider an area (A) of Kapton that is 1cm2. Assume (i) that the flux of AOs (F) is 2.5 x 1020 atoms/cm2/s and (ii) that 3.04 x 10-24 cm3 Kapton is removed per AO (RE: reaction efficiency). Then the rate of loss of film thickness (x) (- dx/dt=A x F x RE) is (3.5x1020 AO/cm2/s) x (3.04 x 10-24 cm3/ AO). What is the rate of Kapton film loss in space? If the film is 1cm thick, how long will it last attack by AOs if the rate remains constant?
AO- atomic oxygen

3)If the rate of adsorption (dθ/dt) is kax p02 x (1-θ) exp (-Ea/RT) what is the time for a 1m2 window to be covered by O2 at an altitude of 300km above the Earth’s surface?

4)Suggest one object that would be better produced in space than on Earth??
 
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Welcome to PF :smile:

You'll have to show an attempt at solving HW problems before receiving help (forum policy).

Also, it's better to make a separate thread for each question. If we had a running discussion involving 4 separate problems in one thread, it could get pretty confusing as to who is talking about which problem.
 


1) If the rate of adsorption (dθ/dt) is kax p02 x (1-θ) exp (-Ea/RT) what is the time for a 1m2 window to be covered by O2 at an altitude of 300km above the Earth’s surface?
 
surrey physical haha
 

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