3.6.13 · D4Spacecraft Structures & Systems Engineering

Exercises — Shock response spectrum (SRS)

3,397 words15 min readBack to topic

Before we start, we reuse a few symbols the parent note earned. Let us restate them in plain words so nothing is unexplained:


Level 1 — Recognition

L1·Q1

Fill each blank by revealing.

The SRS plots
maximum absolute acceleration versus natural frequency
The oscillator model used to build an SRS is a
single-degree-of-freedom (SDOF) mass-spring-damper
The standard damping used for a "Q = 10" system is
(5%)
Recall Solution

These are direct restatements of the Shock response spectrum (SRS) definition. The key relation gives . See Quality factor Q and damping.

L1·Q2

A pyroshock spec is quoted as "1800g at 2000 Hz, ." What does the number 1800g physically represent?

Recall Solution

It is the peak absolute acceleration that a single SDOF oscillator tuned to Hz (with 5% damping, i.e. ) would experience if you drove its base with this shock. It is not the input peak, and not an FFT amplitude — it is the response of one imaginary test oscillator. (This is the core of Mistake 1 in the parent note.)


Level 2 — Application

L2·Q1

An oscillator has Hz. Find (a) in rad/s, (b) the period in ms.

Recall Solution

(a) . What we did / why: counts radians per second, counts whole cycles per second, and one cycle is radians — hence the factor . (b) . This is the time for one full bounce.

L2·Q2

A half-sine shock has amplitude and duration . Using the low-frequency asymptote, estimate the SRS at Hz. First confirm you are allowed to use that formula.

Recall Solution

Step 1 — check the branch. Compute . Since , the oscillator manages only a tenth of a bounce during the pulse — we are firmly on the rising (low-frequency) branch, so the asymptote is valid. Step 2 — plug in. What this means: far below the knee the resonator barely responds — only ~15g out of a 300g input.

Read the figure. Figure s01 below is the SRS of this exact half-sine: horizontal axis is natural frequency in Hz (log scale), vertical axis is the SRS peak acceleration in g (log scale). Find Hz (orange dot) on the left: it sits low on the steep magenta climb, at ≈15g — matching our hand calculation. The violet dashed line marks the knee; everything to its left is the rising branch we just used, and the far-right magenta plateau is the high-frequency limit .

Figure — Shock response spectrum (SRS)

Level 3 — Analysis

L3·Q1

For the same half-sine (), find the knee frequency, and say what happens to the knee if the pulse is made half as long.

Recall Solution

What it means: below ~1.6 kHz you are on the rising branch; above it the curve flattens toward the peak. On the figure above this is exactly where the violet dashed line stands. Halving the pulse: gives — the knee doubles. A shorter, sharper bang pushes the danger zone to higher frequency. This is why Pyroshock environments (very short, sharp) threaten high-frequency components like PCBs and relays.

L3·Q2

Two oscillators sit on the same 300g half-sine ( ms). Oscillator A: Hz. Oscillator B: Hz. Without heavy computation, which sees more acceleration, and why?

Recall Solution

Compute the branch number for each:

  • A: deep on the rising branch.
  • B: right at the knee (). Why B wins: on the rising branch the SRS grows like . B is 4× A's frequency, so on the asymptote alone B would already be higher; and B additionally sits at the knee where the oscillator rings up for nearly a full cycle, adding real amplification. B sees far more.

Read the figure. On figure s01, the navy dot (A: 400 Hz) sits near the flat bottom-left of the climb, while the violet dot (B: 1600 Hz) sits high, right at the knee — a picture of the 16×-plus gap we just argued. Figure s02 shows why: its horizontal axis is time in ms and its vertical axis is normalized response; the navy trace (low ) barely wiggles during the shaded pulse, while the magenta trace (near-knee ) visibly rings up.

Figure — Shock response spectrum (SRS)

Level 4 — Synthesis

L4·Q1

A circuit board has Hz, . A stage-separation event is idealised as a half-sine of peak lasting ms. (a) Which branch is the board on? (b) Estimate its peak acceleration consistently with the low-frequency asymptote. (c) At what would it be worst hit, and what should you do about it?

Recall Solution

(a) Branch. . That is rising branch, so the oscillator hardly moves during the pulse and the response is small (not amplified). (Single-degree-of-freedom systems language: the pulse ends before the board finishes one swing.) (b) Estimate — use the branch's own formula. Because we are on the rising branch, we must use the low-frequency asymptote, not a made-up amplification factor: Compute the pieces: , , product . Then So the board sees only ≈25g, far below the 500g input — exactly what "rising branch" means. (This corrects the tempting but wrong "2×500 = 1000g": a factor above 1 cannot occur this deep on the rising branch.) (c) Worst case. The peak lives near the knee: . A board tuned there would ring up hardest (there, and only there, amplification climbs toward the -limited value). Engineering action: keep the board's well below the knee (as here) — its own dynamics protect it. Danger appears only if a redesign accidentally pushes toward ~637 Hz; then add damping (potting compound raises , capping the peak) or shock-isolate. See Force limiting in shock testing and Shock testing methods.

L4·Q2

A supplier rates a relay at 1500g SRS at 2000 Hz, . Your flight spec is 1800g at 2000 Hz, . (a) Is it qualified? (b) You add an isolator that lowers the relay's effective from 2000 Hz to 800 Hz. Assuming the flight SRS on the rising branch scales as , estimate the new environment the relay would see if the 2000 Hz value (1800g) sits just above the knee and the rising branch reaches 1800g there. Is it qualified now?

Recall Solution

(a) Same (5%), so we compare directly: capability 1500g < requirement 1800g → NOT qualified as-is. (b) Treating the environment as on the rising branch and pinning 1800g at 2000 Hz: Now qualified with margin (margin ). Lowering off the knee dropped the environment dramatically. This is why isolation/soft-mounting is the go-to fix.


Level 5 — Mastery

L5·Q1

Derive the exact low-frequency asymptote for a half-sine, from the dynamics — not from memory. Then check it reproduces the L2·Q2 number.

Recall Solution

Setup — recall the three symbols. is the input base acceleration, the relative displacement (mass position measured from the moving base), and the absolute acceleration that we peak-detect for the SRS. Input half-sine for , then . The base-relative displacement obeys (from the parent EOM, with since damping barely matters this deep on the rising branch):

Why (the justified step). Start from the parent's exact relation . Compare the two terms at the response peak: the free ringing satisfies , so the damping term is — a fraction of the stiffness term. For that is only 6%–10%, negligible for an estimate. Dropping it leaves : the absolute acceleration is set by the spring's stiffness term. (Physically: for a lightly damped oscillator, nearly all the force felt by the mass comes through the spring, and spring force , so acceleration .)

Step 1 — why the pulse acts as an impulse (WHAT/WHY). When , over the whole pulse , so and its restoring term are negligible during the pulse; the equation is essentially . Integrating once, the pulse hands the system a velocity change while leaving (displacement is one more integration of a tiny quantity). What it looks like: the oscillator is standing still, then gets kicked — figure s02, the near-knee trace begins ringing right after the shaded pulse.

Step 2 — free ringing after the kick. For the system rings freely from initial conditions , : Its amplitude is .

Step 3 — impulse-level estimate. Since , the peak is This already proves the SRS is proportional to and vanishes as . But the pure impulse throws away the small correction from not being exactly zero at ; the exact half-sine keeps it, and that correction turns the leading behaviour from into .

Step 4 — exact residual solution (the missing integration). Solve exactly on with . Writing , the particular + homogeneous solution is After the pulse () the motion is free ringing whose amplitude is fixed by . For (i.e. ) expand . Evaluating the post-pulse ring amplitude in this limit gives Cleanly: the residual ring amplitude carries a leading factor (from the term evaluated at the pulse end), and multiplying by the stiffness factor in , then inserting , collapses everything to This is (steeper than the crude impulse ) — the true low-frequency behaviour.

Step 5 — numeric check. At Hz, , ms: matching L2·Q2 exactly. ✓

L5·Q2

Now handle the opposite edge case: the high-frequency plateau (). (a) Explain physically why the SRS flattens and to what value. (b) State the -limited peak that a sustained resonance would reach, and contrast it with the transient half-sine plateau.

Recall Solution

(a) Why it flattens (WHAT/WHY). When the oscillator's period is much shorter than the pulse. During the slow, gentle rise and fall of the base, such a stiff, fast oscillator has time to settle into quasi-static equilibrium with the base at every instant: the mass simply follows the base. Then the relative displacement is small and the component's absolute acceleration equals the base acceleration. Its peak is therefore the input peak: A horizontal line at the input peak — the flat magenta plateau on the far right of figure s01. This is the essential high-frequency edge case: the SRS cannot keep rising forever; it saturates at (a small overshoot bump sits just past the knee before it settles).

(b) The -limited peak (different scenario). If instead the base were driven sinusoidally and forever at exactly (steady-state resonance, not a transient pulse), the response would build up over many cycles to an amplification of For this is — a 10× amplification. Contrast: a short shock pulse never sustains the drive long enough to reach the full ; the half-sine plateau saturates near (amplification ≈1, with a modest overshoot ≈1.7× just past the knee), not . The full only appears for the peak of a long, resonant input — see Quality factor Q and damping. This is why blindly multiplying a shock input by over-predicts the plateau.

Figure — Shock response spectrum (SRS)
Recall One-line summary you should be able to say from memory

Compute first ::: if you are on the quadratic (+12 dB/oct) rising branch and the response is small; near you are at the knee (max amplification); if you are on the flat plateau tracking the input peak .

Related reading: Pyroshock environments · Duhamel's integral · Quality factor Q and damping · MIL-STD-810 Method 516 · Acceleration response in structures · Modal analysis · Mechanical impedance.