Nexø II Rocket Launch Windows Confirmed

Copenhagen Suborbitals Nexø II rocket is 6.7m in length and 0.3m in diameter. Powered by a 5000N thrust LOX/Ethanol liquid rocket engine and guided by jet vanes, the rocket is expected to reach an altitude of 12.6km (41,338.58ft).

You can read more about the Nexø II mission here.

Comments

Fill in your details below or click an icon to log in:

WordPress.com Logo

You are commenting using your WordPress.com account. Log Out /  Change )

Google+ photo

You are commenting using your Google+ account. Log Out /  Change )

Twitter picture

You are commenting using your Twitter account. Log Out /  Change )

Facebook photo

You are commenting using your Facebook account. Log Out /  Change )

Connecting to %s