Science Fair Project Encyclopedia
Lockheed X-17
The Lockheed X-17 was a three stage solid-fuel research rocket to test the effects of high mach reentry.
Service history
The first stage of the X-17 carried the rocket to a height of 17 mi before burning out. The rocket would then coast on momentum to about 100 mi before nosing down for reentry. The second stage engine would then fire before jettisoning and ignighting the thrid and final stage. Ultimately the X-17 would be travelling towards earth at up to Mach 14.5.
Specifications (X-17)
General characteristics
- Length: 40 ft 4 in (12.3 m)
- Wingspan: 7 ft 7 in (2.3 m)
- Diameter:
- 1st stage: 2 ft 7 in (0.79 m)
- 2nd stage: 2 ft 5 in (0.43 m)
- 3rd stage: 0 ft 9.7 in (0.25 m)
- Empty: lb ( kg)
- Loaded: 12,000 lb (5,400 kg)
- Propulsion:
- 1st stage:1x Thiokol XM20 Sergeant solid-fuel rocket, 48,000 lbf (213 kN) for 28s
- 2nd stage:3x Thiokol XM19 Recruit solid-fuel rocket, 33,900 lbf (150 kN) for 1.53s (each)
- 3rd stage:1x Thiokol XM19E1 Recruit solid-fuel rocket, 35,950 lbf (160 kN) for 1.53s
Performance
- Maximum speed: Mach 14.5
- Range: 135 miles (217 km)
- Service ceiling: 250 mi (400 km)
- Rate of climb: ft/min ( m/min)
- Wing loading: lb/ft² ( kg/m²)
External links
Related content
Related development:
Comparable aircraft:
Designation sequence: X-14 - X-15 - X-16 - X-17 - X-18 - X-19 - X-20
See also:
Last updated: 06-02-2005 03:16:22
10-26-2009 08:16:03
The contents of this article is licensed from www.wikipedia.org under the GNU Free Documentation License. Click here to see the transparent copy and copyright details
The contents of this article is licensed from www.wikipedia.org under the GNU Free Documentation License. Click here to see the transparent copy and copyright details