Little Joe 5B

id: little-joe-5b-301-1424485
title: Little Joe 5B
text: 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
brand slug: wiki
category slug: encyclopedia
description:
original url: https://en.wikipedia.org/wiki/Little_Joe_5B
date created:
date modified: 2023-03-21T01:53:48Z
main entity: {"identifier":"Q1814645","url":"https://www.wikidata.org/entity/Q1814645"}
image: {"content_url":"https://upload.wikimedia.org/wikipedia/commons/6/62/Little_Joe_5B_liftoff.jpg","width":4093,"height":4837}
fields total: 13
integrity: 14

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