oss#ome &waterrocket& - tu delft repository45b37689-5752-4ecc-94ca... ·...
TRANSCRIPT
OSS-‐OME #1 WATER ROCKET OSS 1 – Buck, De La Mora, Galvan, Hatun, Kurian, Regondi, Simanjuntak, Swaminathan, Vonwegen, Xu
Mo0va0on (Purpose) Design a water rocket using recycled materials that has the capability to glide in the air for the maximum amount of Ime by ensuring a quick deployment of the parachute to maintain the stability.
Challenges 1. AutomaIc deployment of the parachute 2. The design of the nose cone 3. OpImal air to water raIo
Approach and Innova0ons 1. Installing a plasIc fork to give structural
integrity to the cone while ascending and to hold the strings while descending
2. Reducing the size of the cone to obtain a lighter weight and creaIng a smooth parachute deployment system
3. Parachute folding technique 4. Using 2:1 as the opImal air to water raIo
to gain the maximum thrust
Experiments and Trials Oss-‐ome rocket has only experienced the downfall trial to ensure the parachute deployment system worked as planned. The trials were performed in the outdoors and the wind should affect the flight. 1. First trial – the parachute did not deploy due to the weight of the
nose cone 2. Second trial – the nose cone was successfully detached but the
parachute did not open due to the folding technique 3. Third trial – both the nose cone and parachute deployed as
planned. Also, due to the strong winds, Oss-‐ome rocket was driYed and glided for a longer amount of Ime.
Rocket Materials 1. Thrust chamber: 1.5L recycled plasIc bo[le 2. ConnecIng part: cut-‐off plasIc bo[le 3. Nose cone: recycled paper, plasIc fork, clay 4. Three fins: recycled cardboard 5. Parachute: plasIc and strings 6. Fuel system: pressurized air and water
Result Gliding velocity obtained is 0.67 m/s (esImated).