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D5

Rocket file · LV-297

Delta 5920-8

McDonnell Douglas · Delta · RETIRED

Delta 5920-8 is an expendable launch vehicle built by McDonnell Douglas. It stands 34.0 m tall, lifts 3,848 kg to low Earth orbit, first flew on 18 November 1989. It has flown 1 times with 1 successes, a success rate of 100.0%. It has nothing on the Launch Library 2 schedule right now.

Specification

Vehicle spec sheet

ON FILE
Height34.0 m
Diameter2.4 m
Payload to LEO3,848 kg
Payload to GTO1,405 kg
Maiden flight18 November 1989
ReusableNo, expendable
Launch cost$34.2M
StatusRETIRED

As listed by Launch Library 2. The cost is Launch Library’s figure, not a quoted price. Figures for rockets outside the sixty most-flown were last read on 2026-11-05.

Flight record

Reliability

ON RECORD
Total flights1
Successful1
Failed0
Success rate100.0%
Landing attempts0
Landing successN/A
Scheduled0
Variant5920-8

About Delta 5920-8

The Delta 5000 series was an American expendable launch system which was used to conduct an orbital launch in 1989. It was a member of the Delta family of rockets. Although several variants were put forward, only the Delta 5920 was launched.

Upcoming flights

Manifest

EMPTY

Delta 5920-8 is retired, and no flight is filed.

All upcoming launches

From NASA's public image library and Wikimedia Commons. Each photo shows the credit its licence asks for and links back to where it came from.

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Common questions

How many times has Delta 5920-8 flown?
1 times, with 1 successes and 0 failures.
What is Delta 5920-8's success rate?
100.0%. That's 1 successful flights out of 1 attempts.
How much can Delta 5920-8 lift to orbit?
Launch Library 2 lists Delta 5920-8 at 3,848 kg to low Earth orbit and 1,405 kg to geostationary transfer orbit.
Is Delta 5920-8 reusable?
No. Launch Library 2 lists Delta 5920-8 as expendable, so no stage is recovered to fly again.