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Retired

Pegasus HAPS

Pegasus HAPS

🏭 Orbital Sciences Corporation🌐 American📖 Wikipedia
Pegasus HAPS

The Pegasus is an air-launched rocket developed by Orbital Sciences Corporation (now part of Northrop Grumman Innovation Systems). Capable of carrying small payloads of up to 443 kilograms (977 lb) into low Earth orbit, the vehicle consists of three solid propellant stages and an optional monopropellant fourth stage. Pegasus is released from its carrier aircraft at approximately 40,000 ft (12,000 m), and its first stage has a wing and a tail to provide lift and attitude control while in the atmosphere. The HAPS variant adds a Hydrazine Auxiliary Propulsion System maneuvering stage.

0.3 t
LEO Capacity
15.5 m
Height
2
Total Launches
100.0%
Success Rate

📷 Photo Gallery

Pegasus HAPS photo 1

📊 Specifications

📏Height
15.5 m
⭕Diameter
1.28 m
⚖️Launch Mass
18 kg
🛰️LEO Capacity
250 kg
🌍GTO Capacity
0 kg
🗓️Maiden Flight
Jul 17, 1991
🚀Total Launches
2
✅Success Rate
100%
♻️Reusable
Expendable
🏭Manufacturer
Orbital Sciences Corporation
🌐Country
American
📋Status
Retired