Presentation is loading. Please wait.

Presentation is loading. Please wait.

AEROSPACE 410 AEROSPACE PROPULSION Lecture (9/30/2002) Fi 103 V1-pulse jet powered BUZZ BOMB - 2 PULSE JET ARGUS Dr. Cengiz Camci.

Published byCleopatra Spencer Modified over 9 years ago

Similar presentations

Presentation on theme: "AEROSPACE 410 AEROSPACE PROPULSION Lecture (9/30/2002) Fi 103 V1-pulse jet powered BUZZ BOMB - 2 PULSE JET ARGUS Dr. Cengiz Camci."— Presentation transcript:

1

2 AEROSPACE 410 AEROSPACE PROPULSION Lecture (9/30/2002) Fi 103 V1-pulse jet powered BUZZ BOMB - 2 PULSE JET ARGUS Dr. Cengiz Camci

3 580km/h 45 explosions per sec.

4

5 Spherical air tanks 150 bars (2200 psig) for gyro operation and autopilot Fuel tank at 7 bars ( Fuel tank at 7 bars

6 PULSE JET NOZZLES

7

8 Fuel consumption 0.37 lt/sec. Fuel tank 567 lt Typical flight duration = 1500 seconds=25 minutes At 600 meter altitude

9 Engine weight 153 kg including fuel system Engine performance 390 kg thrust 0 km alt at 750 km/hr 312 kg thrust 1 km alt at 700 km/hr 252 kg thrust 2 km alt at 640 km/hr 202 kg thrust 3 km alt at 560 km/hr

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

26

27 Pilot leaves The jet after The target is sufficiently close This design is not Popular because of Exteremely high Vibration levels (pilot health)

28

Download ppt "AEROSPACE 410 AEROSPACE PROPULSION Lecture (9/30/2002) Fi 103 V1-pulse jet powered BUZZ BOMB - 2 PULSE JET ARGUS Dr. Cengiz Camci."

Similar presentations

1 Lecture 5: Propulsion Jason Mickey For AE 440 A/C Lecture September 2009.

1 Lecture 5: Propulsion Jason Mickey For AE 440 A/C Lecture September 2009.
Analysis of Rocket Propulsion

Analysis of Rocket Propulsion
U3AEA04 ELEMENTS OF AERONAUTICS

U3AEA04 ELEMENTS OF AERONAUTICS
Jet Engines Engine Review Back to School – Spring Break is Over!

Jet Engines Engine Review Back to School – Spring Break is Over!
Introduction to Propulsion

Introduction to Propulsion
AEROSPACE 410 AEROSPACE PROPULSION Lecture HYPER X X-43 project NASA SCRAM-JET TESTS Using a rocket booster from ORBITAL SCIENCES INC. Dr. Cengiz Camci.

AEROSPACE 410 AEROSPACE PROPULSION Lecture HYPER X X-43 project NASA SCRAM-JET TESTS Using a rocket booster from ORBITAL SCIENCES INC. Dr. Cengiz Camci.
Title: Intro to Water Bottle Rockets

Title: Intro to Water Bottle Rockets
Lecture 3b: Aircraft Engines

Lecture 3b: Aircraft Engines
Airplane forces. Weight and Lift WEIGHT – directed to the center of earth – airplane parts, fuel, and people, luggage or freight LIFT – generated by the.

Airplane forces. Weight and Lift WEIGHT – directed to the center of earth – airplane parts, fuel, and people, luggage or freight LIFT – generated by the.
1 Q0 A skydiver jumps off a plane at 3000m. He falls with his belly “facing down” to 1000m altitude before opening up his parachute. Which is the qualitatively.

1 Q0 A skydiver jumps off a plane at 3000m. He falls with his belly “facing down” to 1000m altitude before opening up his parachute. Which is the qualitatively.
The Lander is at a 25 km Lunar altitude and an orbital period of approximately 110 minutes. After separation occurs the Lander is completely self sufficient.

The Lander is at a 25 km Lunar altitude and an orbital period of approximately 110 minutes. After separation occurs the Lander is completely self sufficient.
Introduction to Hypersonic Propulsion Systems

Introduction to Hypersonic Propulsion Systems
Class 4: Fundamentals of Rocket Propulsion

Class 4: Fundamentals of Rocket Propulsion
Gas turbine cycles for aircraft propulsion In shaft power cycles, power is in form of generated power. In air craft cycles, whole power is in the form.

Gas turbine cycles for aircraft propulsion In shaft power cycles, power is in form of generated power. In air craft cycles, whole power is in the form.
OPOC s30 FIS requirement.ppt pg. 1 Combat Propulsion Systems Description of Opposed Piston, Opposed Cylinder (OPOC) s30 Engine 13.5 hp at 6,000 rpm Liquid.

OPOC s30 FIS requirement.ppt pg. 1 Combat Propulsion Systems Description of Opposed Piston, Opposed Cylinder (OPOC) s30 Engine 13.5 hp at 6,000 rpm Liquid.
MAE 4261: AIR-BREATHING ENGINES

MAE 4261: AIR-BREATHING ENGINES
Aerospace 410 Aerospace Propulsion. DESIGN AND DEVELOPMENT OF SMALL TURBO-JET ENGINES THRUST < 100 Lbf Prepared by : Cengiz Camci November 2002.

Aerospace 410 Aerospace Propulsion. DESIGN AND DEVELOPMENT OF SMALL TURBO-JET ENGINES THRUST < 100 Lbf Prepared by : Cengiz Camci November 2002.
Small Propulsion Systems  A 19 lbs thrust “small turbo-jet turbo-shaft gas turbine”  Unusual engines for UAV/MAV applications Dr. Cengiz Camci.

Small Propulsion Systems  A 19 lbs thrust “small turbo-jet turbo-shaft gas turbine”  Unusual engines for UAV/MAV applications Dr. Cengiz Camci.
Takeoff Performance Jet Aircraft Performance

Takeoff Performance Jet Aircraft Performance
Jeff Dennen Justin Marriott Brian Melo Matt Skillin Pulse Jet Engine.

Jeff Dennen Justin Marriott Brian Melo Matt Skillin Pulse Jet Engine.

Similar presentations

Ads by Google