Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
Icarus
American sounding rocket, developed by students at Embry-Riddle Aeronautical University in 2003-2007. Took a 7-kg payload to a 61 km altitude. The Loki Research solid rocket engine had a total mass of 44 kg and an empty mass of 4 kg.
 Status: Active.  First Launch: 2007-03-22.  Last Launch: 2007-03-22.  Number:  1 . Thrust: 15.80 kN (3,552 lbf). Gross mass: 121 kg (266 lb). Specific impulse: 240 s. Burn time: 6.40 s. Height: 4.90 m (16.00 ft). Diameter: 0.15 m (0.49 ft). Apogee: 60 km (37 mi). 
2 stage vehicle consisting of 1 x Icarus + 1 x Icarus Stage 2.
Subtopics
 | Icarus St2 Loki Research solid rocket engine. Icarus second stage. | 
Country: 
USA. 
Propellants: 
Solid. 
Launch Sites: 
Wallops Island. 
Stages: 
Icarus St2. 
Agency: 
ERAU. 
Bibliography: 
2. 
2007 March 22 - . 
10:15 GMT - . 
Launch Site: 
Wallops Island. 
Launch Vehicle: 
Icarus. 
- ERAU / Icarus test - . 
Nation: USA. 
Agency: ERAU. 
Apogee: 60 km (37 mi). 
 
Back to top of page
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2019 Mark Wade - Contact 
© / Conditions for Use