In today's world, Little Joe 5B occupies a central place in our lives. Whether it is politics, technology, history, or any other area of interest, Little Joe 5B is a topic that sparks the interest and curiosity of millions of people around the world. In this article, we will explore different aspects related to Little Joe 5B, delving into its relevance, its impact on society, and the different perspectives that can be had on this topic. From its origins to its evolution today, Little Joe 5B has been the subject of debate, reflection and analysis, and through this article we will seek to shed light on various aspects that surround it.
![]() Launch of Little Joe 5B from Wallops Island | |
Mission type | Abort test |
---|---|
Operator | NASA |
Mission duration | 5 minutes, 25 seconds |
Distance travelled | 14 kilometres (9 mi) |
Apogee | 4.5 kilometres (2.8 mi) |
Spacecraft properties | |
Spacecraft | Mercury No.14 |
Manufacturer | McDonnell Aircraft |
Launch mass | 1,141 kilograms (2,515 lb) |
Start of mission | |
Launch date | April 28, 1961, 14:03 | UTC
Rocket | Little Joe |
Launch site | Wallops LA-4 |
End of mission | |
Landing date | April 28, 1961, 14:08 | UTC
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Little Joe 5B was an uncrewed launch escape system test of the Mercury spacecraft, conducted as part of the US Mercury program. The mission used production Mercury spacecraft # 14A. The mission was launched April 28, 1961, from Wallops Island, Virginia. The Little Joe 5B flew to an apogee of 2.8 miles (4.5 km) and a range of 9 miles (14 km). The mission lasted 5 minutes 25 seconds. Maximum speed was 1,780 mph (2865 km/h) and acceleration was 10 g (98 m/s²). The mission was a success and Mercury spacecraft # 14A was recovered.[1]
Mercury spacecraft #14A used in the Little Joe 5B mission, is on display at the Virginia Air and Space Center in Hampton, Virginia.[2]
This article incorporates public domain material from websites or documents of the National Aeronautics and Space Administration.