NASA Student Launch

Here is a link for the 2023 NASA Student Launch Challenge Results :

https://www.nasa.gov/press-release/nasa-names-winners-of-2023-student-rocket-launch-competition

Yamhill high-school and Camas High-school did AWESOME 👍🙂🚀🚀🚀🏆🏆🏆

NAR Competition NRC Events for the 2022-2023 Contest Year

The NAR Contest Board is pleased to announce the NRC events for the 2022-2023 Contest Year:

A Altitude
A Payload
A Boost/Glide Duration
A Streamer Duration
B Eggloft Duration
1/4A Parachute Duration

These events have been selected by the NAR Contest Board and the NARAM Contest Director per Sporting Code rule 13.1.3. The 2022-2023 Contest Year starts on July 23, 2022 and ends on the last day of NARAM. NRC flying ends June 30, 2023.

Dan Wolf
NAR Contest Board Chair

2022-23 NRC Contest Events Announced

Approved Altimeters

Contest Advice

http://www.nar.org/contest-flying/competition-guide/nar-rocketry-competition/

For information on the new contest book, here is the link:

https://www.nar.org/wp-content/uploads/2021/06/USMRSC_May-2021.pdf

If you have any questions please feel free to contact:

gorgerc790@gmail.com

Board of Trustee Meetings/Town Hall Meetings

Daniel Peirce did a remarkable job with the Semroc Saturn 1B rocket

Check out the rocketry show at https://www.therocketryshow.com/ — Check out the rocketry show at
https://www.therocketryshow.com/

http://wgvunews.org/post/national-association-rocketry-festival

http://www.spacesounds.com/

"Congratulations to Daniel Peirce for Certifying Level 1"

Daniel successfully launched his Mad Cow Honest John rocket on an H128-10W with great results:

Welcome to the Gorge Rocket Club Section 790 website.

If you have any questions please feel free to contact me: Thompsonje@gmail.com

My Background

What is Thrust to weight ratio?

To safely launch a rocket the thrust to weight ratio should be at least 5 to 1

For example, if a rocket weighs 0.4 kg, and the motor has a thrust of 15 Newtons, is this safe?

Answer: The weight of the rocket is 0.4 x 9.8 = 3.9 N. Thrust is 15 N. The thrust to weight ratio is thus 15:3.9, or 3.8:1. This is less than 5:1 so the launch would be unsafe.

http://apollo17.org/

http://www.nar.org/