Zhuque-2 baseline configuration
The baseline Zhuque-2 was the original 49.5-metre configuration flown on Y1 through Y3. Four TQ-12 engines powered the first stage; the second stage used a TQ-12 main engine and a smaller TQ-11 vernier engine. The first flight failed, while Y2 and Y3 reached orbit before the program transitioned to Zhuque-2E.
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Identity
- Aliases
- ZQ-2 baselineZhuque-2 basic modelZhuque-2 Y1-Y3 configuration朱雀二号基本型
- Family Name
- Zhuque-2
- Full Name
- Zhuque-2 baseline configuration
- Status
- retired
- Type
- rocket
- Variant Name
- Baseline
Details
- Description
- The baseline Zhuque-2 was the original 49.5-metre configuration flown on Y1 through Y3. Four TQ-12 engines powered the first stage; the second stage used a TQ-12 main engine and a smaller TQ-11 vernier engine. The first flight failed, while Y2 and Y3 reached orbit before the program transitioned to Zhuque-2E.
- Dimensions
- Diameter M
- 3.35
- Height M
- 49.5
- First Flight Year
- 2,022
- Last Flight Year
- 2,023
- Manufacturer
- Operator
- Parent Vehicle Family
- Propulsion Configurations
- Entries
- Nested value
- Nested value
- Nested value
- Rocket Specs
- Liftoff Mass Kg
- 220,000
- Reusability
- expendable
- Stages Count
- 2
- Strap On Boosters Count
- 0
Links
Assets & Meta
- Creation Time
- July 14, 2026 at 06:02:15 UTC
- Updated Time
- July 29, 2026 at 15:43:16 UTC
- Image
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- Search Name
- Zhuque-2 baseline configuration ZQ-2 baseline Zhuque-2 basic model Zhuque-2 Y1-Y3 configuration 朱雀二号基本型