DOC: update readme

README.md

@@ -7,18 +7,18 @@
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 [![Open In Colab](https://colab.research.google.com/assets/colab-badge.svg)](https://colab.research.google.com/github/RocketPy-Team/rocketpy/blob/master/docs/notebooks/getting_started_colab.ipynb)
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 [![Documentation Status](https://readthedocs.org/projects/rocketpyalpha/badge/?version=latest)](https://docs.rocketpy.org/en/latest/?badge=latest)
+[![PyPI](https://img.shields.io/pypi/v/rocketpy?color=g)](https://pypi.org/project/rocketpy/)
+![Conda Version](https://img.shields.io/conda/v/conda-forge/rocketpy?color=g)
 [![codecov](https://codecov.io/gh/RocketPy-Team/RocketPy/graph/badge.svg?token=Ecc3bsHFeP)](https://codecov.io/gh/RocketPy-Team/RocketPy)
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 [![Contributors](https://img.shields.io/github/contributors/RocketPy-Team/rocketpy)](https://github.com/RocketPy-Team/RocketPy/graphs/contributors)
-[![Chat on Discord](https://img.shields.io/discord/765037887016140840?logo=discord)](https://discord.gg/b6xYnNh)
 [![Sponsor RocketPy](https://img.shields.io/static/v1?label=Sponsor&message=%E2%9D%A4&logo=GitHub&color=%23fe8e86)](https://github.com/sponsors/RocketPy-Team)
+[![Chat on Discord](https://img.shields.io/discord/765037887016140840?logo=discord)](https://discord.gg/b6xYnNh)
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-<br>
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 # RocketPy
 
 RocketPy is the next-generation trajectory simulation solution for High-Power Rocketry. The code is written as a [Python](http://www.python.org) library and allows for a complete 6 degrees of freedom simulation of a rocket's flight trajectory, including high-fidelity variable mass effects as well as descent under parachutes. Weather conditions, such as wind profiles, can be imported from sophisticated datasets, allowing for realistic scenarios. Furthermore, the implementation facilitates complex simulations, such as multi-stage rockets, design and trajectory optimization and dispersion analysis.
@@ -80,6 +80,9 @@ Flight data and rocket parameters used in this comparison were kindly provided b
 |   NDRT launch vehicle   | Apogee time (s)        |    16.77  |    17.10  |   **-1.90 %**   |
 |   NDRT launch vehicle   | Maximum velocity (m/s) |   172.86  |   168.95  |   **2.31 %**    |
 
+Over years of development and testing, RocketPy has been validated across an expanding range of flight scenarios.
+For more information on these validated flights, visit our [Flight Examples](https://docs.rocketpy.org/en/latest/examples/index.html) page in the documentation.
+
 # Documentation
 
 Check out documentation details using the links below:
@@ -161,7 +164,7 @@ env = Environment(
     latitude=32.990254,
     longitude=-106.974998,
     elevation=1400,
-) 
+)
 
 tomorrow = datetime.date.today() + datetime.timedelta(days=1)
 
@@ -352,7 +355,7 @@ You can also become a [sponsor](https://github.com/sponsors/RocketPy-Team) and h
 
 If you are actively using RocketPy in one of your projects, reaching out to our core team via [Discord](https://discord.gg/b6xYnNh) and providing feedback can help improve RocketPy a lot!
 
-And if you are interested in going one step further, please read [CONTRIBUTING.md](https://github.com/RocketPy-Team/RocketPy/blob/master/CONTRIBUTING.md) for details on our code of conduct and learn more about how you can contribute to the development of this next-gen trajectory simulation solution for rocketry.
+And if you are interested in going one step further, please read the [development documentation](https://docs.rocketpy.org/en/latest/development/index.html) to learn more about how you can contribute to the development of this next-gen trajectory simulation solution for rocketry.
 
 ## License