×
We have recently moved to a new server. If you run into any issues, please let us know through the Contact Us link at the bottom of the page. Thanks for visiting RocketReviews.
UCLA Rocket Project static firing the HyPE 1A Test Engine. Fuel is aluminized paraffin, oxidizer is nitrous oxide. There was a problem with the nitrogen pressurization system which prevented the engine from starting properly. The cause is believed to have been a seized check valve. Nominal thrust is 1000 lbs, this test peaked at 200 lbs.