Team Icarus SRM Test

Team Icarus, a team under the SDSU Rocket Project, recently tested their in-house designed and built solid rocket motor. The motor is intended to launch a boosted dart to 100,000ft.

This particular motor was a 4″ dia (101.2mm) composite case, burning an APCP propellant blend, producing a chamber pressure of 760psi. The burn time was 5sec.

You can follow Team Icarus on Facebook to stay up to date on this project.

Advertisements

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 )

Twitter picture

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

Facebook photo

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

Google+ photo

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

Connecting to %s