Data[]
Statistic. | Data. |
---|---|
Type. | Atmospheric re-entry testing unit. |
Height. | 40 ft 4 in (12.3 m). |
Diameter. | 1st stage: 2 ft 7 in (0.79 m), 2nd stage: 1 ft 5 in (0.43 m) and 3rd stage: 0 ft 9.7 in (0.25 m). |
Weight. | 3,400 kg (7,400 lb). |
Payload. | Some weighted test probes, cameras and senors. |
Speed. | Mach 14.5. |
Steering. | N\A, but probably akin to aircraft of comparable role, configuration and era. |
Nationality. | American. |
Made by. | Lockheed Corporation. |
Guidance system. | N\A. |
Maximum altitude gained. | 500 km (310 mi). |
Range. | 135 miles (217 km). |
First made. | 1955. |
Fist used. | 1955. |
Retied on. | 1958. |
Thrust. | 220.00 kN (49,450 lbf). |
Engines | N\A, but probably akin to those of comparable role, configuration and era. |
Sources | http://www.designation-systems.net/dusrm/app1/x-17.html, http://users.dbscorp.net/jmustain/x-17.htm, http://en.wikipedia.org/wiki/Lockheed_X-17, http://www.astronautix.com/x/x-17.html and http://www.astronautix.com/lvs/x17.htm |
- Wingspan- 7 ft 7 in (2.3 m).
The idea[]
To create a successor to the Astrobee rocket and Black Brant I rocket.
History[]
The Lockheed X-17 was a three stage solid-fuel research rocket to test the effects of high mach atmospheric re-entry. It took off from Patrick AFB at one point and reached the speed of Mach 14.5.
The X-17 was also used as the booster for the Operation Argus series of three high-altitude nuclear tests that were conducted in the South Atlantic during 1958.
Technical note[]
Whist it was puny in comparison to other later rockets, both it and other related rockets like the unguided suborbital sounding rocket, the Astrobee rocket and the Black Brant I rocket rocket were, non the less, a vital stage in researching early space data such as how high speeds and extreme g-forces would affect aviation machinery.
Also see[]
- Saturn V rocket
- Vostok 1 rocket
- Bell Textron Rocket Belt
- Bell Pogo
- KGB Chita Jet Belt
- Bell X-1
- North American X-15
- Patrick Air Force Base
- American X-aircraft